;-------------------------------------------------------------------------------
; #alert "alert text goes here - if uncommented, it will be displayed in a pop-up dialog whenver a project using this INI is opened"
; INI date: Aug.28/11 6:52AM PDT

#  set AUTO_TRIG
#  unset MS2_SEQ
[MegaTune]
   MTversion      = 2.25 ; MegaTune itself; needs to match exec version.

   versionInfo    = "S"  ; Put this in the title bar.
   queryCommand   = "Q"  ; Verify against signature.
   signature      = "MSII Rev 3.77000   " ; MS-II sends a null at 20th byte.
                   ; 123456789.123456789.

;-------------------------------------------------------------------------------
;
; PREAMBLE
;
; There are several main sections (with brackets around the [section] heading) in this INI file:
;
; - Constants - this is divided into two pages (for recent MS-II code versions, 
;               at least). Page 1 is based on the source code inpram. structure
;               Page 2 is based on the source code in2ram. structure. All of the 
;               values are inputs sent from MegaTune to the MegaSquirt-II
; - Menu (& User Defined) - these define most of the mennus in MegaTune (except 
;                           those that are 'built-in' like the accel wizrd, etc.)
; - Curve Editor and Table Editor
; - Gauge Configuration
; - Front Page & RuntTime & Tuning Config
; - Burst Mode Config
; - Output Channels - this mirrors the outpc. structure from the source code. All 
;                     of the values are sent from MegaSquirt-II to MegaTune on the PC.
; - Datalog - select output channels to log on the PC hard drive
;
; Note: 
;       - To add an input variable to MegaTune, you need to add it to the inpram (or in2ram) 
;         structure in the MegaSquirt source code noting the correct offset (and recompile, 
;         of course), to the Constants section, and to one of the menus.
;       - To add an output variable to MegaTune (for monitoring, logging, or switching purposes),
;         you need to add it to the outpc structure in the source code, to the OuptChannels, and 
;         to the datalog section (and/or the gauge configurations, if you wish to see it directly 
;         in MegaTune). 
;
; In general, the respective notation for variables from the source code to the INI are:
;
;                         signed          unsigned      bytes    bits
;                         ------          --------      -----    ----
;             - char =      S08              U08          1       8
;             - int  =      S16              U16          2       16
;             - long =      S32              U32          4       32
;
; Where the maximum range is:
;
;                         signed           unsigned
;                         ------           --------
;             - char =   -128 to 127       0 to 255
;             - int  =   -32768 to 32767   0 to 65535
;             - long =   -2147483648       0 to 4294967295        
;                         to 2147483647
;
;----------------------------------------------------------------------------
; Temperature Limits and Settings Reference
;----------------------------------------------------------------------------
;
; Below is a listing of all of the temperature ranges used throughout the INI for the MegaSquirt II.
;
; CELSIUS (Expanded/Normal):
;     Low limit: -40C/-40C
;     High limit: 300C/150C
;     Low danger: 65C/10C
;     Low warning: 93C/65C
;     High warning: 162C/93C
;     High danger: 176C/104C
;
; FAHRENHEIT (Expanded/Normal):
;     Low Limit: -40F/-40F
;     High limit: 600F/300F
;     Low danger: 150F/50F
;     Low warning: 200F/150F
;     High warning: 325F/200F
;     High danger: 350F/220F
;----------------------------------------------------------------------------


[ReferenceTables]

    tableWriteCommand 	= "t" ; 
    
    referenceTable = mafTableBurner, "Calibrate MAF Table..."
    	;topicHelp = "http://www.megamanual.com/mt29.htm#om"
        tableIdentifier = 003, "MAF Table"
        adcCount 	= 1024 	; length of the table
        bytesPerAdc 	= 2 	; using words
        scale		= 1 ; scale before sending to controller
        ;tableGenerator	= Generator Type, 		Label, xUnits, yUnits,  xLow, xHi,  yLow, yHi ; lows and Hi's are just default values, they will be user editable
    	;tableGenerator	= linearGenerator, "Custom Linear WB", "Volts","AFR",    1,   4,   9.7,  18.7
    	solutionsLabel	= "MAF Sensor"
    	solution	= "Ford Lightning MAF", 	{ table(adcValue, "maffactor_1L3F_Lightning.inc") }
		solution	= "Infiniti Q45 MAF", 		{ table(adcValue, "maffactor_Q45.inc") }
		solution	= "GM LT1/LS1/LS2 MAF", 	{ table(adcValue, "maffactor_lsx.inc") }

    referenceTable = canOutmsgBurner, "Configure CAN Outmsg"
    	;topicHelp = "http://www.megamanual.com/mt29.htm#outmsg"
        tableIdentifier = 010, "outmsg Table"       ; id in octal, 010 = table 8
        adcCount 	= 1024 	; length of the table
        bytesPerAdc 	= 1 	; using bytes
        scale		= 1 ; scale before sending to controller
        ;tableGenerator	= Generator Type, 		Label, xUnits, yUnits,  xLow, xHi,  yLow, yHi ; lows and Hi's are just default values, they will be user editable
    	;tableGenerator	= linearGenerator, "Custom Linear WB", "Volts","AFR",    1,   4,   9.7,  18.7
    	solutionsLabel	= "CAN Outmsg"
    	solution	= "CAN Outmsg", 	{ table(adcValue, "canOutmsg.inc") }


[Constants]

   ;----------------------------------------------------------------------------
   ; Constants Definition
   ; --------------------
   ;
   ; Scalar Values
   ; -------------
   ; The scaling and translation values are used as follows:
   ;    msValue   = userValue / scale - translate
   ;    userValue = (msValue + translate) * scale
   ;
   ; I've got no good way to handle a few of these things yet.
   ;
   ; Temperatures are fine, check out the Fielding IAC example (fastIdleTemp).
   ;
   ; The TPS stuff is a problem, because we have to modify the INI file for
   ; each TPS installation and again whenever we move the TPS...
   ;
   ; Array Values
   ; ------------
   ; Arrays are specified just like scalars, except that they have a "shape"
   ; entry in the fourth parameter.  The shape allows you to define lists or
   ; tables, for example [8] defines a list with eight values and [2x4] defines
   ; a table with eight values (two rows and four columns).  Tables may be
   ; stored in either "X-" or "Y-order."  X-order means that memory is laid
   ; out as follows:
   ;
   ;     [x1,y1] [x2,y1]...[xn,y1] [x1,y2]...
   ;
   ; Y-order would be
   ;
   ;     [x1,y1] [x1,y2]...[x1,yn] [x2,y1]...
   ;
   ; To use the TableEditor, you must define two lists and a table, and
   ; the lengths of the lists must correspond to the shape of the table.
   ;
   ; Bit Fields
   ; ----------
   ; Bits are numbered 0-7, the rightmost being bit zero.  The basic
   ; data word that stores bit fields must be unsigned.
   ;
   ; You need NOT supply the correct number of labels matching the
   ; number of bits you've specified (one bit requires 2 values, two
   ; bits requires 4 values and so on).  If you neglect to supply enough
   ; labels, they will be synthesized using the sequence "1", "2" and so
   ; on based upon their position in the sequence (the cltType and matType
   ; will end up with identical lists).
   ;
   ;----------------------------------------------------------------------------

   pageActivationDelay =  50 ; Milliseconds delay after burn command.
   blockReadTimeout    = 200 ; Milliseconds total timeout for reading page.

   endianness          = big
   nPages              = 2
   pageSize            = 996,            954
   pageIdentifier      = "\x00\x04",     "\x00\x05"
   burnCommand         = "b%2i",         "b%2i"
   pageReadCommand     = "r%2i%2o%2c",   "r%2i%2o%2c"
   pageValueWrite      = "w%2i%2o%2c%v", "w%2i%2o%2c%v"
   pageChunkWrite      = "w%2i%2o%2c%v", "w%2i%2o%2c%v"

   page = 1
   ;  name            = class,  type, offset,      shape,  units,       scale, translate,    lo,      hi, digits
      nCylinders      = bits  ,  U08,      0,      [0:3], "INVALID"                                              ; *
      no_skip_pulses  = scalar,  U08,      1,             "",         1.00000,   0.00000,  1.00,  255.00,      0 ; * (  1 byte )
      ICIgnCapture    = bits  ,  U08,      2,      [0:0], "Falling Edge", "Rising Edge"                          ; *
#if MS2_SEQ
      ICCrankTrigger  = bits  ,  U08,      2,      [1:2], "Calculated", "INVALID", "INVALID",    "INVALID" ; *
#else
      ICCrankTrigger  = bits  ,  U08,      2,      [1:2], "Calculated", "Trigger Return", "Trigger Rise",    "INVALID" ; *
#endif

#if MS2_SEQ
      ICIgnOption     = bits  ,  U08,      2,      [4:5], "Standard Coil Charge", "INVALID", "INVALID", "INVALID" ; *
#else
      ICIgnOption     = bits  ,  U08,      2,      [4:5], "Standard Coil Charge", "EDIS", "EDIS Multispark", "INVALID" ; *
#endif      
      spkout_hi_lo    = bits  ,  U08,      3,      [0:0], "Going Low (Normal)", "Going High (Inverted)"          ; *
      max_coil_dur    = scalar,  U08,      4,             "msec",     0.10000,   0.00000,  1.00,    8.00,      1 ; * (  1 byte )
      max_spk_dur     = scalar,  U08,      5,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
      dwellAcc        = scalar,  U08,      6,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
      dwellVolts      = array ,  S08,      7,    [    5], "V",        0.10000,   0.00000,-12.80,   12.70,      1 ; * (  5 bytes)
      dwellDuration   = array ,  S08,     12,    [    5], "msec",     0.10000,   0.00000,-12.80,   12.70,      1 ; * (  5 bytes)
      RevLimOption    = bits  ,  U08,     17,      [0:1], "None", "Spark Retard", "Fuel Cut", "Soft Fuel Cut"    ; * (  1 byte )
      RevLimMaxRtd    = scalar,  U08,     18,             "deg",      0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte ) 
      PredOpt         = bits  ,  U08,     19,      [0:1], "Last Interval", "Alpha-Beta-Gamma Filter", "INVALID", "INVALID" ; *
      crankingRPM     = scalar,  S16,     20,             "RPM",      1.00000,   0.00000,  0.00,  3000.0,      0 ; * (  2 bytes)
      cold_adv_table  = array ,  S16,     22,    [   10], "deg",      0.10000,   0.00000,-10.00,   10.00,      1 ; * ( 20 bytes)
      triggerOffset   = scalar,  S16,     42,             "deg",      0.10000,   0.00000,-359.0,  359.00,      2 ; * (  2 bytes)
      RevLimRpm1      = scalar,  S16,     44,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      RevLimRpm2      = scalar,  S16,     46,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
#if LAMBDA
      afrTable1       = array ,  U08,     48,    [12x12], "Lambda",  0.006803,   0.00000,  0.00,    2.00,      3 ; * (144 bytes)
      afrTable2       = array ,  U08,    192,    [12x12], "Lambda",  0.006803,   0.00000,  0.00,    2.00,      3 ; * (144 bytes)
#else
      afrTable1       = array ,  U08,     48,    [12x12], "AFR",      0.10000,   0.00000,  9.00,   20.00,      1
      afrTable2       = array ,  U08,    192,    [12x12], "AFR",      0.10000,   0.00000,  9.00,   20.00,      1
#endif
      wueBins         = array ,  U08,    336,    [   10], "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * ( 10 bytes)
      taeBins         = array ,  U08,    346,    [    4], "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  4 bytes)
      maeBins         = array ,  U08,    350,    [    4], "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  4 bytes)
      iacstepTable    = array ,  S16,    354,    [   10], "steps",    1.00000,   0.00000,  0.00, 4000.00,      0 ; * ( 20 bytes)
      ipwmTable       = array ,  S16,    354,    [   10], "%",        1.00000,   0.00000,  0.00,  100.00,      0
      frpm_table      = array ,  U16,    374,    [   12], "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * ( 24 bytes)
      srpm_table      = array ,  U16,    398,    [   12], "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * ( 24 bytes)
      fmap_table      = array ,  S16,    422,    [   12], "kPa",      0.10000,   0.00000,  0.00,  400.00,      1 ; * ( 24 bytes)
      smap_table      = array ,  S16,    446,    [   12], "kPa",      0.10000,   0.00000,  0.00,  400.00,      1 ; * ( 24 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      tempTable       = array ,  S16,    470,    [   10], "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * ( 20 bytes) Temperature bins for cranking, cold AE and WUE
  #else  
      tempTable       = array ,  S16,    470,    [   10], "°C",       0.05555,  -320.000,-40.00,  100.00,      1 ; * ( 20 bytes) Temperature bins for cranking, cold AE and WUE
  #endif  
#else
  #if EXPANDED_CLT_TEMP
      tempTable       = array ,  S16,    470,    [   10], "°F",       0.10000,   0.00000,-40.00,  600.00,      1
  #else
      tempTable       = array ,  S16,    470,    [   10], "°F",       0.10000,   0.00000,-40.00,  200.00,      1
  #endif
#endif
      taeRates        = array ,  S16,    490,    [    4], "%/sec",    1.00000,   0.00000,  0.00, 32767.0,      0 ; * (  8 bytes) tpsDot bins used for AE: x for TAE interpolation
      maeRates        = array ,  S16,    498,    [    4], "kPa/sec",  1.00000,   0.00000,  0.00, 32767.0,      0 ; * (  8 bytes) mapDot bins used for AE: x for MAE
      map0            = scalar,  S16,    506,             "kPa",      0.10000,   0.00000, -100.0, 3276.7,      1 ; * (  2 bytes)
      mapmax          = scalar,  S16,    508,             "kPa",      0.10000,   0.00000, -100.0, 3276.7,      1 ; * (  2 bytes)
#if CELSIUS
      clt0            = scalar,  S16,    510,             "°C",       0.05555,  -320.000, -100.0,  500.0,      1 ; * (  2 bytes)
      cltmult         = scalar,  S16,    512,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ; * (  2 bytes)
      mat0            = scalar,  S16,    514,             "°C",       0.05555,  -320.000, -100.0,  500.0,      1 ; * (  2 bytes)
#else
      clt0            = scalar,  S16,    510,             "°F",       0.10000,   0.00000, -100.0,  500.0,      1
      cltmult         = scalar,  S16,    512,             "%",        1.00000,   0.00000, -200.0,  200.0,      0
      mat0            = scalar,  S16,    514,             "°F",       0.10000,   0.00000, -100.0,  500.0,      1
#endif
      matmult         = scalar,  S16,    516,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ; * (  2 bytes)
      tpsMin          = scalar,  S16,    518,             "ADC",      1.00000,   0.00000,    0.0, 1023.0,      0 ; * (  2 bytes)
      tpsMax          = scalar,  S16,    520,             "ADC",      1.00000,   0.00000,    0.0, 1023.0,      0 ; * (  2 bytes)
      batt0           = scalar,  S16,    522,             "V",        0.10000,   0.00000,    0.0, 3276.7,      1 ;   (  2 bytes)
      battmax         = scalar,  S16,    524,             "V",        0.10000,   0.00000,-3276.8, 3276.7,      1 ;   (  2 bytes)
      ego0            = scalar,  S16,    526,             "afr",      0.10000,   0.00000,-3276.8, 3276.7,      1 ;   (  2 bytes)
      egomult         = scalar,  S16,    528,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ;   (  2 bytes)
      baro0           = scalar,  S16,    530,             "kPa",      0.10000,   0.00000,-3276.8, 3276.7,      1 ; * (  2 bytes)
      baromax         = scalar,  S16,    532,             "kPa",      0.10000,   0.00000,-3276.8, 3276.7,      1 ; * (  2 bytes)
      bcor0           = scalar,  S16,    534,             "%",        1.00000,   0.00000,-3276.8, 3276.7,      1 ; * (  2 bytes)
      bcormult        = scalar,  S16,    536,             "%",        1.00000,   0.00000, -200.0,  200.0,      0 ; * (  2 bytes)
      knock0          = scalar,  S16,    538,             "V",        0.01000,   0.00000,    0.0,    5.0,      1 ; * (  2 bytes)
      knockmax        = scalar,  S16,    540,             "V",        0.01000,   0.00000,    0.0,    5.0,      1 ; * (  2 bytes)
#if MS2_SEQ
      CPWOption       = bits,    U08,    542,      [0:1], "no cranking pulses", "sequential crank pulses", "simultaneous crank pulses", "INVALID"  ;  * (  1 byte)
#else
      CPWOption       = bits,    U08,    542,      [0:1], "no cranking pulses", "simultaneous crank pulses", "INVALID", "INVALID"  ;   * (  1 byte)
#endif
      Cam_Tooth       = scalar,  U08,    543,             "teeth",    1.00000,   0.00000,  0.00,  127.00,      0 ; * (  1 bytes)
      crankTolerance  = scalar,  U08,    544,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      asTolerance     = scalar,  U08,    545,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      pulseTolerance  = scalar,  U08,    546,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      IdleCtl         = bits  ,  U08,    547,      [0:2], "None", "Solenoid", "IAC Stepper Moving Only", "IAC Stepper Always On", "PWM Warmup", "15-Minute IAC", "INVALID", "INVALID" ; *
      IACtstep        = scalar,  U08,    548,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
      IACaccstep      = scalar,  U08,    549,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
      IACminstep      = scalar,  U08,    550,          "steps",       1.00000,   0.00000,  1.00,  255.00,      0 ; * (  1 byte )
      IACpwm_step     = scalar,  U08,    551,             "Hz",      80.00000,   0.00000, 80.00,  800.00,      0 ; * (  1 byte )
      IACStart        = scalar,  S16,    552,          "steps",       1.00000,   0.00000,  0.00, 4000.00,      0 ; * (  1 byte )
#if CELSIUS
      IdleHyst        = scalar,  S16,    554,             "°C",       0.05555,   0.00000,   0.0,   30.0,       1 ; * (  2 bytes)
#else
      IdleHyst        = scalar,  S16,    554,             "°F",       0.10000,   0.00000,   0.0,   50.0,       1
#endif
      IACcrankpos     = scalar,  S16,    556,             "steps",    1.00000,   0.00000,  0.00, 4000.00,      0 ; * (  2 bytes)
      IACcrankxt      = scalar,  S16,    558,             "sec",      1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      IACcoldtmp      = scalar,  S16,    560,             "°C",       0.05555,  -320.000, -40.0,  300.0,       1 ; * (  2 bytes)
  #else
      IACcoldtmp      = scalar,  S16,    560,             "°C",       0.05555,  -320.000, -40.0,  150.0,       1 ; * (  2 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      IACcoldtmp      = scalar,  S16,    560,             "°F",       0.10000,   0.00000,-40.00,  500.00,      1
  #else
      IACcoldtmp      = scalar,  S16,    560,             "°F",       0.10000,   0.00000,-40.00,  300.00,      1
  #endif
#endif
      IACcoldpos      = scalar,  S16,    562,             "steps",    1.00000,   0.00000,  0.00, 4000.00,      0 ; * (  2 bytes)
      IACcoldxt       = scalar,  S16,    564,             "sec",      1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
      primePulseCold  = scalar,  S16,    566,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  2 bytes)
      primePulseHot   = scalar,  S16,    568,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  2 bytes)
      crankCold       = scalar,  S16,    570,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  1 byte )
      crankHot        = scalar,  S16,    572,             "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * (  1 byte )
      asePctCold      = scalar,  S16,    574,             "%",        1.00000,   0.00000,  0.00,  400.00,      0 ; * (  2 bytes)
      asePctHot       = scalar,  S16,    576,             "%",        1.00000,   0.00000,  0.00,  400.00,      0 ; * (  2 bytes)
      aseCountCold    = scalar,  S16,    578,             "cycles",   1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
      aseCountHot     = scalar,  S16,    580,             "cycles",   1.00000,   0.00000,  0.00,32767.00,      0 ; * (  2 bytes)
      taeColdA        = scalar,  U08,    582,             "msec",     0.10000,   0.00000,  0.00,  25.500,      1 ; * (  1 byte )
      taeColdM        = scalar,  U08,    583,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      tpsThresh       = scalar,  U08,    584,             "%/sec",    1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      mapThresh       = scalar,  U08,    585,             "kPa/sec",  1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte ) threshold for MAE
      taeTime         = scalar,  U08,    586,             "sec",      0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
      tdePct          = scalar,  U08,    587,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      floodClear      = scalar,  S16,    588,             "%",        0.10000,   0.00000,  0.00,  100.00,      1 ; * (  2 bytes)
      TPSOXLimit      = scalar,  S16,    590,             "%",        0.10000,   0.00000,  0.00,  100.00,      1 ; * (  2 bytes)
      tpsProportion   = scalar,  U08,    592,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte )
      baroCorr        = bits  ,  U08,    593,      [0:1], "None", "Initial MAP Reading", "Two Independent Sensors", "INVALID"        ; *
      egoType         = bits  ,  U08,    594,      [0:2], "Disabled", "Narrow Band", "Dual Narrow Band", "Wide Band", "Dual Wide Band", "Dual NB on AD7", "Dual WB on AD7", "INVALID" ; *
      egoCount        = scalar,  U08,    595,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      egoDelta        = scalar,  U08,    596,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      egoLimit        = scalar,  U08,    597,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
#if   NARROW_BAND_EGO
      AFRTarget       = scalar,  U08,    598,             "v",        0.01000,   0.00000,  0.00,    2.00,      4 ; * (  1 byte )
#elif LAMBDA
      AFRTarget       = scalar,  U08,    598,             "Lambda",   0.006803,  0.00000,  0.00,   2.00,      3
#else
      AFRTarget       = scalar,  U08,    598,             "AFR",      0.10000,   0.00000,  0.00,   25.50,      1
#endif
      tempUnits       = bits  ,  U08,    599,      [0:0], "Coolant/IAT Tables in °F", "Coolant/IAT Tables in °C"  ; * (  1 byte )
      MAFOption       = bits  ,  U08,    600,      [0:1], "No MAF",  "MAF Only", "MAF/MAP blend", "MAF, MAP mfld/cyl model",      ; * 
      MAFpin          = bits  ,  U08,    600,      [4:5], "MAF on MAP pin", "MAF on Baro Pin", "MAF on Knock Pin", "INVALID" ; *
      MAFtype         = bits  ,  U08,    600,      [7:7], "Voltage MAF", "Frequency MAF"  ; *
#if MS2_SEQ 
      DualSpkOptn     = bits  ,  U08,    601,      [0:3], "INVALID", "INVALID", "Falling Cam Sync with Crank Wheel", "Rising Cam Sync with Crank Wheel", "Single Crank Wheel Input", "Single Cam Wheel Input", "INVALID", "M-0 Wheel w/ Falling Crank Sync", "M-0 Wheel w/ Rising Crank Sync", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID" ; * (1 byte)
#else
      DualSpkOptn     = bits  ,  U08,    601,      [0:3], "No Dual/Multi Spark", "Dual Tach Inputs", "Falling Cam Sync with Tach or Wheel", "Rising Cam Sync with Tach or Wheel", "Single Crank Wheel Input", "Single Cam Wheel Input", "Dual Inputs, Timing from 1 cam tooth", "M-0 Wheel w/ Falling Crank Sync", "M-0 Wheel w/ Rising Crank Sync", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID", "INVALID" ; * (1 byte)
#endif
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      fastIdleT       = scalar,  S16,    602,             "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * (  2 bytes)
      egoTemp         = scalar,  S16,    604,             "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * (  2 bytes)
  #else
      fastIdleT       = scalar,  S16,    602,             "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * (  2 bytes)
      egoTemp         = scalar,  S16,    604,             "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * (  2 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      fastIdleT       = scalar,  S16,    602,             "°F",       0.10000,   0.00000,-40.00,  600.00,      1
      egoTemp         = scalar,  S16,    604,             "°F",       0.10000,   0.00000,-40.00,  600.00,      1
  #else
      fastIdleT       = scalar,  S16,    602,             "°F",       0.10000,   0.00000,-40.00,  300.00,      1
      egoTemp         = scalar,  S16,    604,             "°F",       0.10000,   0.00000,-40.00,  300.00,      1
  #endif
#endif
      egoRPM          = scalar,  S16,    606,             "RPM",      1.00000,   0.00000,  0.00, 15000.0,      0 ; * (  2 bytes)
      reqFuel         = scalar,  U16,    608,             "msec",     0.00100,   0.00000,  0.00,  65.536,      2 ; * (  2 bytes)
      divider         = scalar,  U08,    610,             "",         1.00000,   0.00000,  0.00,     255,      0 ; * (  1 byte )
#if MS2_SEQ
      alternate       = bits,    U08,    611,      [0:0], "Simultaneous", "INVALID"                              ; * (  1 byte )
#else
      alternate       = bits,    U08,    611,      [0:0], "Simultaneous", "Alternating"                          ; * (  1 byte )
#endif
      injOpen         = scalar,  U08,    612,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
#if MS2_SEQ
      injPwmT         = scalar,  U08,    613,             "msec",     0.10000,   0.00000,  25.5,   25.50,      1 ; * (  1 byte )
      injPwmPd        = scalar,  U08,    614,             "µsec",     1.00000,   0.00000, 40.00,  100.00,      0 ; * (  1 byte )
      injPwmP         = scalar,  U08,    615,             "%",        1.00000,   0.00000, 100.0,  100.00,      0 ; * (  1 byte )
#else
      injPwmT         = scalar,  U08,    613,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
      injPwmPd        = scalar,  U08,    614,             "µsec",     1.00000,   0.00000, 40.00,  100.00,      0 ; * (  1 byte )
      injPwmP         = scalar,  U08,    615,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte)
#endif
      battFac         = scalar,  U08,    616,             "ms/v",     0.0166667, 0.00000,  0.00,    1.00,      2 ; * (  1 byte )
#if MS2_SEQ
      twoStroke       = bits,    U08,    617,      [0:0], "Four-stroke",    "INVALID"                            ; *
      injType         = bits,    U08,    618,      [0:0], "Port Injection", "INVALID"                            ; *
#else
      twoStroke       = bits,    U08,    617,      [0:0], "Four-stroke",    "Two-stroke"                         ; *
      injType         = bits,    U08,    618,      [0:0], "Port Injection", "Throttle Body"                      ; *
#endif
      nInjectors      = bits,    U08,    619,      [0:4], "INVALID"                                              ; *
      OddAng          = scalar,  S16,    620,      "degrees",         0.10000,   0.00000,-700.0,  700.00,      1
      rpmLF           = scalar,  U08,    622,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      mapLF           = scalar,  U08,    623,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      tpsLF           = scalar,  U08,    624,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      egoLF           = scalar,  U08,    625,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      adcLF           = scalar,  U08,    626,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      knkLF           = scalar,  U08,    627,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      AMCOption       = bits,    U08,    628,      [0:1], "Disabled", "RAM Update", "FLASH Update", "INVALID"    ; * (  1 byte ) 
      dualTable       = bits,    U08,    629,      [0:1], "Use First VE, Afrtgt Table", "Dual Tables (for each Inj Bank)","Use Second VE, Afrtgt Table","INVALID"  ; *
      algorithm       = bits,    U08,    630,      [0:1], "Speed Density", "Blend SD/AlphaN, PW=--f(tps)xVE(tps,rpm)", "Blend SD/AlphaN, PW=--VE(tps,rpm)", "INVALID" ; *
      alphDir         = bits,    U08,    630,      [4:4],   "Use Above", "Invert Above"                          ; *
      alpha_baro_spkadv = scalar, U08,   631,             "deg/kPa",  0.01000,   0.00000,  0.00,  255.00,      2 ; * (  1 byte )
      AfrAlpha        = scalar,  U08,    632,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; U (  1 byte ) UNUSED
      NBVStoich       = scalar,  U08,    633,             "Volts",    0.01000,   0.00000,  0.00,    7.00,      3 ; * (  1 byte )
      alpha_lorpm     = scalar,  S16,    634,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      alpha_hirpm     = scalar,  S16,    636,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      alphaMAPtable   = array ,  S16,    638,    [ 6x 6], "kPa",      0.10000,   0.00000,  0.00,  200.00,      1 ; * ( 72 bytes)
      amap_tps        = array ,  S16,    710,    [    6], "%",        0.10000,   0.00000,   0.0,  100.00,      1 ; * ( 12 bytes)
      amap_rpm        = array ,  U16,    722,    [    6], "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * ( 12 bytes)
      baud            = scalar,  U32,    734,             "",         1.00000,   0.00000,9600.0,115200.0,      0 ; x (  4 bytes)
      MAPOXLimit      = scalar,  S16,    738,             "kPa",      0.10000,   0.00000,  0.00,  300.00,      2 ; * (  2 bytes)
      board_type      = scalar,  U08,    740,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      mycan_id        = scalar,  U08,    741,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )               
      fet_delay       = scalar,  U08,    742,             "µsec",     1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      vr_delay        = scalar,  U08,    743, "µsec/1000rpm",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )   
#if MS2_SEQ
      ECUType         = scalar,  U08,    744, "1=MS-II, 2=MicroSquirt, 3=Sequencer",   1.00000,   0.00000,  3.00,    3.00,  0 ; * (  1 byte )
#else
      ECUType         = scalar,  U08,    744, "1=MS-II, 2=MicroSquirt, 3=Sequencer",   1.00000,   0.00000,  0.00,    9.00,  0 ; * (  1 byte )
#endif
      MapThreshXTD2   = scalar,  U08,    745,    "-kpa/sec",          1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )

#if n2o
      n2oEnrich       = scalar,  U08,    746,             "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
#else
      pwImpulse       = scalar,  U08,    746,             "msec",     0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte )
#endif

      impulseSec      = scalar,  U08,    747,             "sec",      1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      nImpulse        = scalar,  U08,    748,             "",         1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      airdotSample    = scalar,  U08,    749,             "msec",     1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      tpsdotSample    = scalar,  U08,    750,             "msec",     1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte ) 
      ASEHot          =   bits,  U08,    751,      [0:0], "Disable ASE on Hot Start", "Enable ASE on Hot Start"
      ;pad            = scalar,  U08,    752,             "%",        1.00000,   0.00000,  0.00,  99.00,       0 ; * (  1 byte ) 
      MapThreshXTD    = scalar,  U08,    753,             "-kpa/sec", 1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      MapThreshXTA    = scalar,  U08,    754,             "kpa/sec",  1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      trendmapLimit   = scalar,  U08,    755,             "kpa",      1.00000,   0.00000,  0.00,  255.00,      0 ; * (  1 byte )
      ; Port Settings constants
      psEnabled       = array ,  U08,    756,    [    7], "on/off",   1.00000,   0.00000,   0.00,    1.00,     0 ; * (  2 bytes)
      psCondition     = array ,  U08,    763,    [  7x2], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psConnector     = array ,  U08,    777,    [    7], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psInitValue     = array ,  U08,    784,    [    7], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psPortValue     = array ,  U08,    791,    [    7], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psOutSize       = array ,  U08,    798,    [  7x2], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psOutOffset     = array ,  U16,    812,    [  7x2], "",         1.00000,   0.00000,-128.00,  127.00,     0 ; * (  2 bytes)
      psThreshold     = array ,  U16,    840,    [  7x2], "",         1.00000,   0.00000,-32768.0,32767.0,     0 ; * (  4 bytes)
      psHysteresis    = array ,  U16,    868,    [  7x2], "",         1.00000,   0.00000,-32768.0,32767.0,     0 ; * (  4 bytes)
      aeTaperTime     = scalar,  U08,    896,             "sec",      0.10000,   0.00000,  0.00,   25.50,      1 ; * (  1 byte)
      AFRMult         = bits,    U08,    897,      [0:1], "Use Combined VE/AFR table", "Separate VE & AFR table w/ NB EGO", "Separate VE & AFR table w/ WB EGO", "INVALID"  ; * (  1 byte)
      aeEndPW         = scalar,  S16,    898,             "msec",       0.10000,   0.00000,  0.00, 1000.00,      1 ; *
      egoAlgorithm    = bits  ,  U08,    900,      [0:1], "Simple", "Transport Delay", "PID/Smith Predictor", "INVALID" ; * (  1 byte )
      egoKP           = scalar,  U08,    901,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte )
      egoKI           = scalar,  U08,    902,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte )
      egoKD           = scalar,  U08,    903,             "%",        1.00000,   0.00000,  0.00,  100.00,      0 ; * (  1 byte )
      egoKdelay1      = scalar,  U16,    904,             "msec",     1.00000,   0.00000,  0.00,   65535,      0 ; * (  2 bytes)
      egoKdelay2      = scalar,  U16,    906,             "revs",     1.00000,   0.00000,  0.00,   65535,      0 ; * (  2 bytes)
      flexFuel        = bits  ,  U08,    908,      [0:1], "Disabled", "FlexFuel Sensor", "FlexFuel Switch", "INVALID"  ; * (  1 byte )
      prime_delay     = scalar,  U08,    909,             "sec",      1.00000,   0.00000,  0.00,     255,      0 ; * (  1 byte )
      fuelFreq        = array ,  U08,    910,    [    2], "Hz",       1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
         fuelFreq0    = scalar,  U08,    910,             "Hz",       1.00000,   0.00000,  0.00,     255,      0
         fuelFreq1    = scalar,  U08,    911,             "Hz",       1.00000,   0.00000,  0.00,     255,      0
      fuelCorr        = array ,  U08,    912,    [    2], "%",        1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
         fuelCorr0    = scalar,  U08,    912,             "%",        1.00000,   0.00000,  0.00,     255,      0
         fuelCorr1    = scalar,  U08,    913,             "%",        1.00000,   0.00000,  0.00,     255,      0
      AMCstep         = scalar,  U08,    914,             "%",        1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
      AMCdve          = scalar,  U08,    915,             "%",        1.00000,   0.00000,  0.00,     255,      0 ; * (  2 bytes)
      AMCve_rpm       = scalar,  U16,    916,             "RPM",      1.00000,   0.00000,  0.00,15000.00,      0 ; * (  2 bytes)
      AMCve_map       = scalar,  U16,    918,             "kPa",      0.10000,   0.00000,  0.00,  300.00,      2 ; * (  2 bytes)
      AMCramve_dt     = scalar,  U16,    920,             "sec",      1.0,       0.0,      0.0,   300.0,       0 ; * (  2 bytes)
      AMCT_thresh     = scalar,  U16,    922,             "sec",      1.0,       0.0,      0.0,  1800.0,       0 ; * (  2 bytes)
      AMCupdate_thresh= scalar,  U16,    924,             "events",   1.0,       0.0,      0.0, 30000.0,       0 ; * (  2 bytes)
      CWOption        = bits  ,  U08,    926,      [0:0], "Two-Point", "Table"                                   ; * (  1 byte )
      knkOption       = bits  ,  U08,    927,      [0:1], "Disabled", "Safe Mode", "Aggressive Mode", "INVALID"  ; * (  1 byte )
      knkDirection    = bits  ,  U08,    927,      [4:4], "Below threshold", "Above threshold"                   ; *
      knk_maxrtd      = scalar,  U08,    928,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_step1       = scalar,  U08,    929,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_step2       = scalar,  U08,    930,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_trtd        = scalar,  U08,    931,             "sec",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_tadv        = scalar,  U08,    932,             "sec",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_dtble_adv   = scalar,  U08,    933,             "deg",      0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      knk_ndet        = scalar,  U08,    934,             "knocks",   1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
     ;pad             = scalar,  U08,    935,
      knk_maxmap      = scalar,  U16,    936,             "kPa",      0.1,       0.0,      0.0,   300.0,       1 ; * (  2 bytes)
      knk_lorpm       = scalar,  U16,    938,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      knk_hirpm       = scalar,  U16,    940,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      knk_rpm         = array ,  U16,    942,    [    6], "rpm",      1.0,       0.0,      0.0,    6000,       0 ; * (  2 bytes)
      knk_thresh      = array ,  U16,    954,    [    6], "v",        0.01,      0.0,      0.0,    5.00,       2 ; * (  2 bytes)
      triggerTeeth    = scalar,  U16,    966,             "teeth",    1.0,       0.0,      0.0,     512,       0 ; * (  2 bytes)
      No_Miss_Teeth   = scalar,  U08,    968,             "teeth",    1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
#if AUTO_TRIG
#else
      No_Skip_Teeth   = scalar,  U08,    969,             "teeth",    1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
      Delay_Teeth     = scalar,  U08,    970,             "teeth",    1.0,       0.0,      0.0,     255,       0 ; * (  1 byte )
#endif
      ICISR_tmask     = scalar,  U08,    971,             "msec",     0.1,       0.0,      0.0,    25.5,       1 ; * (  1 byte )
      ICISR_pmask     = scalar,  U08,    972,             "%",        1.0,       0.0,      0.0,     200,       0 ; * (  1 byte )
      injTestMode     = bits  ,  U08,    973,      [0:1], "Normal Mode", "Test Mode", "Repeat Test", "INVALID"   ;   (  1 byte )
      ae_lorpm        = scalar,  U16,    974,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      ae_hirpm        = scalar,  U16,    976,             "rpm",      1.0,       0.0,      0.0,   10000,       0 ; * (  2 bytes)
      fuelSpkDel      = array ,  S16,    978,    [    2], "deg",      0.10000,   0.00000,-45.00,   45.00,      1 ; * (  4 bytes)
         fuelSpkDel0  = scalar,  S16,    978,             "deg",      0.10000,   0.00000,-45.00,   45.00,      1 ;   (  2 bytes)
         fuelSpkDel1  = scalar,  S16,    980,             "deg",      0.10000,   0.00000,-45.00,   45.00,      1 ;   (  2 bytes)
      injTestSqrts    = scalar,  U16,    982,             "squirts",  1,         0,           0,   65000,      0 ;   (  2 bytes)
      injTestPW       = scalar,  U16,    984,             "msec",     0.001,     0,           0,      65,      3 ;   (  2 bytes)
      injTestOffTime  = scalar,  U16,    986,             "msec",     0.1,       0,           0,    6500,      1 ;   (  2 bytes)
      CID             = scalar,  U16,    988,             "cu.in.",   1,         0,           0,     700,      1 ;   (  2 bytes)         
      alpha           = scalar,  U08,    990,             "%",        1.0,       0.0,        50,     150,      0 ; * (  1 byte ) 
      beta            = scalar,  U08,    991,             "%",        1.0,       0.0,       0.0,     100,      0 ; * (  1 byte )
      gamma           = scalar,  U08,    992,             "%",        1.0,       0.0,       0.0,      50,      0 ; * (  1 byte )
      acc_synchk      = bits,    U08,    993,      [0:1], "Check Only at Steady Speed", "Check Accel and Steady Speed", "Check Decel and Steady Speed", "Check Always" ;  (1 byte)      
      tie1_2cyl       = bits,    U08,    994,      [0:0], "Separate Ign1,2", "Tie Ign1,2 together"               ;   (  1 byte )        
      autoTrig        = bits,    U08,    995,      [0:0], "Disable Auto Trigger", "Enable Auto Trigger"          ;   (  1 byte )        
  
;     pageSize =  996

   page = 2
      veTable1        = array ,  U08,      0,    [12x12], "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (144 bytes)
      veTable2        = array ,  U08,    144,    [12x12], "%",        1.00000,   0.00000,  0.00,  255.00,      0 ; * (144 bytes)
      advanceTable    = array ,  S16,    288,    [12x12], "deg",      0.10000,   0.00000,-10.00,   90.00,      1 ; * (288 bytes)
      AMCNBurns       = scalar,  U16,    576,             "burns",    1,         0,           0,   65000,      0 ; x (  2 bytes)
      primePWTable    = array ,  S16,    578,    [   10], "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * ( 20 bytes)
      crankPWTable    = array ,  S16,    598,    [   10], "msec",     0.10000,   0.00000,  0.00,   65.00,      1 ; * ( 20 bytes)
      asePctTable     = array ,  S16,    618,    [   10], "%",        1.00000,   0.00000,  0.00,  400.00,      0 ; * (  2 bytes)
      aseCntTable     = array ,  S16,    638,    [   10], "cycles",   1.00000,   0.00000,  0.00, 2500.00,      0 ; * (  2 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      matTemps        = array ,  S16,    658,    [    6], "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * ( 12 bytes)
  #else
      matTemps        = array ,  S16,    658,    [    6], "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * ( 12 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      matTemps        = array ,  S16,    658,    [    6], "°F",       0.10000,   0.00000,-40.00,  600.00,      1 ;   (  2 bytes)
  #else
      matTemps        = array ,  S16,    658,    [    6], "°F",       0.10000,   0.00000,-40.00,  300.00,      1 ;   (  2 bytes)
  #endif
#endif
      matRetard       = array ,  U08,    670,    [    6], "deg",      0.10000,   0.00000,  0.00,    25.5,      1 ; * (  6 bytes)
      xTauOption      = bits  ,  U08,    676,      [0:1], "Off", "Accel/Decel Only", "AE with WE", "INVALID"        ; * (  1 byte )
      spkN2O          = scalar,  U08,    677,             "deg",      0.10000,   0.00000,  0.00,    25.5,      1 ; * (  1 bytes)
      XAccTable       = array,   U16,    678,     [   5], "%",        0.10000,   0.00000,  0.00,      90,      1 ; * ( 10 bytes)
      TauAccTable     = array,   U16,    688,     [   5], "msec",     1.00000,   0.00000,  2.00,   20000,      0 ; * ( 10 bytes)
      XDecTable       = array,   U16,    698,     [   5], "%",        0.10000,   0.00000,  0.00,      90,      1 ; * ( 10 bytes)
      TauDecTable     = array,   U16,    708,     [   5], "msec",     1.00000,   0.00000,  2.00,   20000,      0 ; * ( 10 bytes)
      XTrpms          = array,   U16,    718,     [   5], "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * ( 10 bytes)
      XClt            = array,   U16,    728,     [  10], "%",        1.00000,   0.00000,  0.00,     600,      0 ; * ( 20 bytes)
      TauClt          = array,   U16,    748,     [  10], "%",        1.00000,   0.00000,  0.00,     600,      0 ; * ( 20 bytes)
      ftrim           = array,   S16,    768,     [   8],   "%",      0.10000,   0.00000, -200.0,    200.0,    1 ; * ( 16 bytes)
      strim           = array,   S16,    784,     [   8], "deg",      0.10000,   0.00000, -180.0,    180.0,    1 ; * ( 16 bytes) 
#if AUTO_TRIG
#else
     spark_fuel_offset = scalar,U08,    800,             "cyl",      1.00000,   0.00000,  0.00,       7,      0 ; * (  1 bytes) 
#endif
      seq_ack         = scalar,  U08,    801,                "",      1.00000,   0.00000,  0.00,     255,      0 ; * (  1 bytes) 	  
      nskpCPW         = scalar,  U08,    802,                "",      1.00000,   0.00000,  0.00,     255,      0 ; * (  1 bytes)
      mafLF           = scalar,  U08,    803,              "",        1.00000,   0.00000,  0.00,    6000,      0 ; * (  1 bytes) 
      fRate           = scalar,  U16,    804,             "g/s",      0.00100,   0.00000,  0.00,   60000,      3 ; * ( 2 bytes)
      Vmfld           = scalar,  U16,    806,             "cu.cm.",   1.00000,   0.00000,  0.00,   10000,      1 ; * ( 2 bytes)         
      maf_tlag        = scalar,  U16,    808,             "ms",       0.10000,   0.00000,  0.00,    1000,      1 ; * ( 2 bytes)         
      VOF             = scalar,  U08,    810,             "deg/m",    0.01000,   0.00000,  0.00,    4.00 ,     2 ; * (  1 bytes) 
      CR              = scalar,  U08,    811,             "cr",       0.10000,   0.00000,  1.00,      50,      1 ; * (  1 bytes) 
      VERGMOptn       = bits,    U08,    812,      [0:1], "No VE Res Gas Model", "Calc VE Res Gas Model", "Use VE RGM", "VE RGM x VE Tbl" ; * (  1 byte)
; cpad
      c1rgm           = scalar,  U16,    814,             "",         0.00100,   0.00000,  0.00,   6.000,      3 ; * (  2 bytes)
      c2rgm           = scalar,  U16,    816,             "",         0.00100,   0.00000,  0.00,  12.000,      3 ; * (  2 bytes)
      tachoPW         = scalar,  U08,    818,             "ms",       0.12800,   0.00000,  0.00,    25.5,      1 ; * (  1 bytes)
      tachoDuty       = scalar,  U08,    819,             "%",        1.00000,   0.00000,  0.00,     255,      0 ; * (  1 bytes)
#if AUTO_TRIG
      InjStart        = scalar,  U16,    820,           "deg",        0.10000,   0.00000,  0.00,  719.90,      1 ; * (  2 bytes)       
#else
      InjStart        = scalar,  U16,    820,             "%",        1.00000,   0.00000,  0.00,   99.00,      0 ; * (  2 bytes)       
#endif
      mapSample       = scalar,  U16,    822,           "deg",        0.10000,   0.00000,  0.00,  719.90,      1 ; * (  2 bytes)       
      mafSample       = scalar,  U16,    824,           "deg",        0.10000,   0.00000,  0.00,  719.90,      1 ; * (  2 bytes)       
      AFRStoich       = scalar,  U08,    826,           "afr",        0.10000,   0.00000,  0.00,     255,      1 ; * (  1 byte)
      AFRStoichFF     = scalar,  U08,    827,           "afr",        0.10000,   0.00000,  0.00,     255,      1 ; * (  1 byte)
      ipada           = array,   U16,    828,    [17],    "",         1.00000,   0.00000,  0.00,     255,      0 ; * ( 34 bytes)
      activate_xrate_0  = bits,  U08,    862,    [0:0],  "N/A",  "msg 0"                                                ; * ( 2 bytes)
      activate_xrate_1  = bits,  U08,    862,    [1:1],  "N/A",  "msg 1"                                                ; * ( 2 bytes)
      activate_xrate_2  = bits,  U08,    862,    [2:2],  "N/A",  "msg 2"                                                ; * ( 2 bytes)
      activate_xrate_3  = bits,  U08,    862,    [3:3],  "N/A",  "msg 3"                                                ; * ( 2 bytes)
      activate_xrate_4  = bits,  U08,    862,    [4:4],  "N/A",  "msg 4"                                                ; * ( 2 bytes)
      activate_xrate_5  = bits,  U08,    862,    [5:5],  "N/A",  "msg 5"                                                ; * ( 2 bytes)
      activate_xrate_6  = bits,  U08,    862,    [6:6],  "N/A",  "msg 6"                                                ; * ( 2 bytes)
      activate_xrate_7  = bits,  U08,    862,    [7:7],  "N/A",  "msg 7"                                                ; * ( 2 bytes)
	  
      ; Supplemental corrections for barometer and IAT.
      baroCorrVals    = array ,  S16,    864,    [    6], "kPa",      0.10000,   0.00000,  80.0,  120.00,      1 ; * ( 24 bytes)
#if CELSIUS
  #if EXPANDED_CLT_TEMP
      matCorrTemps    = array ,  S16,    876,    [    6], "°C",       0.05555,  -320.000,-40.00,  300.00,      1 ; * ( 12 bytes)
  #else
      matCorrTemps    = array ,  S16,    876,    [    6], "°C",       0.05555,  -320.000,-40.00,  150.00,      1 ; * ( 12 bytes)
  #endif
#else
  #if EXPANDED_CLT_TEMP
      matCorrTemps    = array ,  S16,    876,    [    6], "°F",       0.10000,   0.00000,-40.00,  600.00,      1 ;   (  2 bytes)
  #else
      matCorrTemps    = array ,  S16,    876,    [    6], "°F",       0.10000,   0.00000,-40.00,  300.00,      1 ;   (  2 bytes)
  #endif
#endif
      baroCorrDelta   = array ,  S08,    888,    [    6], "%",        1.00000,   0.00000,-100.0,   120.0,      1 ; * (  6 bytes)
      matCorrDelta    = array ,  S08,    894,    [    6], "%",        1.00000,   0.00000,-100.0,   120.0,      1 ; * (  6 bytes)
      MAFFlow         = array ,  U16,    900,    [   12], "gram/sec", 0.01000,   0.00000,  0.00,   650.0,      1 ; * ( 24 bytes)      
      MAFCor          = array ,  U08,    924,    [   12], "%",        1.00000,   0.00000,  0.00,   255.0,      0 ; * ( 12 bytes)   
      MAFRPM1         = scalar,  U16,    936,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)
      MAFRPM2         = scalar,  U16,    938,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)
      MAFDir          = bits  ,  U08,    940,      [0:0], "Use Above", "Invert Above"                            ; * (  1 byte )
      VEIXOptn        = bits  ,  U08,    941,      [0:1], "Use MAP only", "Adjust MAP for Baro", "Use SAE Pid 43 Abs Load", "INVALID"  ; * (  1 byte )
      MatRtdRPMHi     = scalar,  U16,    942,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)  
      MatRtdRPMLo     = scalar,  U16,    944,             "rpm",      1.00000,   0.00000,  0.00,   10000,      0 ; * (  2 bytes)
      FuelAdj         = scalar,  S16,    946,             "%",        0.10000,   0.00000,  0.00,    1000,      1 ; * (  2 bytes)
      SpkAdj          = scalar,  S16,    948,             "deg",      0.10000,   0.00000,  0.00,    1000,      1 ; * (  2 bytes)
      IdleAdj         = scalar,  S16,    950,             "step",     1.00000,   0.00000,  0.00,    1000,      0 ; * (  2 bytes)
      SprAdj          = scalar,  S16,    952,             "",         1.00000,   0.00000,  0.00,    1000,      1 ; * (  2 bytes)

;     pageSize =  954

[Menu]

   ;----------------------------------------------------------------------------
   ;  There are five pre-defined values that may be used to define your menus.
   ;  The first four allow access to the "standard" dialog boxes, the last one
   ;  merely draws a separator (horizontal line) in the menu.
   ;
   ;     std_constants
   ;     std_enrichments
   ;     std_realtime
   ;     std_warmup
   ;     std_accel
   ;
   ;     std_separator
   ;
   ;  Additionally, to support MegaSquirt-II firmware, there are two standard
   ;  dialogs to generate its three embedded tables.  The first of these acts
   ;  like Roger Enns' EasyTherm, but only works for MS-II.  The second one
   ;  generates the internal AFR table required for proper closed loop operation
   ;  in MS-II.  Use these without page numbers, as they will just be ignored
   ;  in any case.
   ;
   ;     std_ms2gentherm
   ;     std_ms2geno2
   ;
   ;  If you use any of the std_constants, std_enrichments or std_warmup
   ;  editors, they may be optionally suffixed with a page number (only
   ;  useful for multi-page code variants), which causes them to edit the
   ;  specified page.  If you leave off the page specifier, they edit logical
   ;  page one as specified in the Constants section.
   ;
   ;  There are four special menu names, which when used append to the standard
   ;  menus of the same name instead of creating a new one.  The menu names
   ;  are "File", "Communications", "Tools" and "Help".
   ;
   ;----------------------------------------------------------------------------

   menuDialog = main
      menu = "Fuel &Set-Up"
         subMenu = generalSettings, "&General"
         subMenu = idleControl,     "I&dle Control",                   0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_port_edit,   "Spare &Port Settings",            0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = can_activate,    "Activate CAN Out Messages",       0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_separator,   ;----------------------------------------------
         subMenu = injChars,        "I&njector Characteristics",       0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_injection,   "Injection &Control",              0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = revLimiter,      "&Rev Limiter",                    0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = aseSettings,     "Start/&After&Start Enrichment" ,  0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = accSettings,     "Acce&l Enrichment Config",        0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = baroCorrection,  "2-Point &Barometric Correction",  0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = flexFuelSettings,"&Flex Fuel",                      0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = egoControl,      "&EGO Control",                    0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}

	menuDialog = main
     menu = "Other Fue&l Set-Up"	
         subMenu = amcSettings,        "Automatic &Mixture Control",   0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}	 
	 subMenu = alphaNOptions,      "&Alpha-N Blending",            0,  { algorithm  > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
	 subMenu = MAFSettings,        "MAP vrs. MAF &Usage",          0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
	 subMenu = samplerate,         "&Sampling and Smoothing",      0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = otherFuel,          "&Other Fuel Settings",         0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
		 
   menuDialog = main
       menu = "&Ignition Set-Up"
         subMenu = ignitionOptions, "&Base Ignition Settings",         0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = dwellSettings,   "D&well Settings",                 0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = tachSettings,   "Tach Signal Settings",             0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = dualmultisparkoptions, "Dual/Multi Spark Options",  0,  { ECUType == 1 || ECUType == 2 || ECUType == 3} 
         subMenu = AdvncdignitionOptions, "&Advanced Ignition Options",0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = knockSettings,  "&Knock Setup",                     0,  { ECUType == 1 || ECUType == 2}		 
         subMenu = knockThresholdCurve, "K&nock Threshold",            0,  { ECUType == 1 || ECUType == 2} 

   menuDialog = main
      menu = "B&asic Tables"

#if MAPbaro
	 subMenu = std_separator    ;----------------------------------------------
         subMenu = veTable1Tbl,     "&VE Table 1 (MAP/Baro)",         0,  { (MAFOption == 0 || MAFOption == 2) && (dualTable < 2) && (flexFuel != 2) && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = afrTable1Tbl,    "&AFR Table 1 (MAP/Baro)",        0,  { VEIXOptn == 1 && (dualTable < 2) && (flexFuel != 2) }
         subMenu = veTable2Tbl,     "V&E Table 2 (MAP/baro)",         0,  { (MAFOption == 0 || MAFOption == 2) && (dualTable > 0) && (flexFuel != 2) && VEIXOptn == 1 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = afrTable2Tbl,    "AFR &Table 2 (MAP/Baro)",        0,  { VEIXOptn == 1 && (dualTable > 0) && (flexFuel != 2) }
         subMenu = ignitionTbl,     "&Spark Advance Table (MAP/Baro)",0,  { VEIXOptn == 1  && (ECUType == 1 || ECUType == 2 || ECUType == 3)}

#else
         subMenu = veTable1Tbl,     "VE Table &1 (MAP or PID43)",              0,  { (MAFOption == 0 || MAFOption == 2) && (dualTable < 2) && (flexFuel != 2) && VEIXOptn != 1 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = afrTable1Tbl,    "A&FR Table 1 (MAP or PID43)",             0,  { VEIXOptn != 1 && (dualTable < 2) && (flexFuel != 2) }
         subMenu = veTable2Tbl,     "VE Table &2 (MAP or PID43)",              0,  { (MAFOption == 0 || MAFOption == 2) && (dualTable > 0) && (flexFuel != 2) && VEIXOptn != 1 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = afrTable2Tbl,    "AF&R Table 2 (MAP or PID43)",             0,  { VEIXOptn != 1 && (dualTable > 0) && (flexFuel != 2) }
         subMenu = ignitionTbl,     "S&park Advance Table (MAP or PID43)",     0,  { VEIXOptn != 1  && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
#endif
  
     menuDialog = main
      menu = "Othe&r Tables" 
         subMenu = tempTableBins,   "&Temperature Table Values",      0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = alphaMAPTbl,     "&Alpha-N MAP Table",             0,  { algorithm > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = barometerCorr,   "Barometric &Correction",         0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_separator    ;----------------------------------------------   
         subMenu = primingPW,       "Pri&ming Pulse",                 0,  { CWOption > 0  && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = crankingPW,      "Cra&nking Pulse",                0,  { CWOption > 0  && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = asePct,          "A&SE Percentage",                0,  { CWOption > 0  && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = aseTaper,        "AS&E Taper",                     0,  { CWOption > 0  && (ECUType == 1 || ECUType == 2 || ECUType == 3)}

   menuDialog = veTable1Tbl
      menu = "&Edit Bins"
	 subMenu = fmapTableBins,   "Edit Fuel &MAP Bins"
	 subMenu = frpmTableBins,   "Edit Fuel &RPM Bins"

   menuDialog = veTable2Tbl
      menu = "&Edit Bins"
	 subMenu = fmapTableBins,   "Edit Fuel &MAP Bins"
	 subMenu = frpmTableBins,   "Edit Fuel &RPM Bins"


   menuDialog = ignitionTbl
      menu = "&Edit Bins"
	 subMenu = smapTableBins,   "Edit Spark &MAP Bins"
	 subMenu = srpmTableBins,   "Edit Spark &RPM Bins"		 

   menuDialog = main
      menu = "&Tuning"
         subMenu = std_realtime,    "&Realtime Display",              0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}

#if MAPbaro
         subMenu = std_separator    ;----------------------------------------------
         subMenu = veTable1Map,     "VE &Table 1 (MAP/Baro)",         0, { (MAFOption == 0 || MAFOption == 2) && (dualTable < 2) && (flexFuel != 2) && VEIXOptn == 1} 
         subMenu = veTable2Map,     "VE T&able 2 (MAP/Baro)",         0, { (MAFOption == 0 || MAFOption == 2) && (dualTable > 0) && (flexFuel != 2) && VEIXOptn == 1}
         subMenu = afrTable1Map,    "A&FR Ta&ble 1 (MAP/Baro)",       0, { VEIXOptn == 1 && (dualTable < 2) && (flexFuel != 2)}
         subMenu = afrTable2Map,    "A&FR Tabl&e 2 (MAP/Baro)",       0, { VEIXOptn == 1 && (dualTable > 0) && (flexFuel != 2)}
         subMenu = ignitionMap,     "I&gnition Advance Table (MAP/Baro)",    0, { VEIXOptn == 1}

#else
         subMenu = std_separator    ;----------------------------------------------
         subMenu = veTable1Map,     "VE Table &1 (MAP or PID43)",              0, { (MAFOption == 0 || MAFOption == 2) && (dualTable < 2) && (flexFuel != 2) && VEIXOptn != 1} 
         subMenu = veTable2Map,     "VE Table &2 (MAP or PID43)",              0, { (MAFOption == 0 || MAFOption == 2) && (dualTable > 0) && (flexFuel != 2) && VEIXOptn != 1}
         subMenu = afrTable1Map,    "A&FR Table 1 (MAP or PID43)",             0, { VEIXOptn != 1 && (dualTable < 2) && (flexFuel != 2)}
         subMenu = afrTable2Map,    "AF&R Table 2 (MAP or PID43)",             0, { VEIXOptn != 1 && (dualTable > 0) && (flexFuel != 2)}
         subMenu = ignitionMap,     "&Spark Advance Table (MAP or PID43)",     0, { VEIXOptn != 1}
#endif

         subMenu = std_separator    ;----------------------------------------------
         subMenu = std_warmup,      "&Warmup Wizard",                 0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_accel,       "Acce&leration Wizard",           0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}   

 
   menuDialog = main
       menu = "C&ylinder Trims"   
         subMenu = fueltrim,        "Fuel Trim Percentages",          0, { DualSpkOptn && ((nCylinders <= 2) || (ECUType == 3)) }
         subMenu = sparktrim,       "Spark Trim Degrees",             0, { DualSpkOptn && ((nCylinders <= 2) || (ECUType == 3)) }

   menuDialog = main
       menu = "X-Ta&u Tuning"
         subMenu = XAccTable,       "Puddling Factors (&accel)",      0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = XDecTable,       "Puddling Factors (&decel)",      0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = TauAccTable,     "Time Factors (a&ccel)",          0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = TauDecTable,     "Time Factors (d&ecel)",          0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = XCltTable,       "&X (Puddling) Temp. Corrections",0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}    
         subMenu = TCltTable,       "&Tau (Time) Temp. Corrections",  0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = std_separator    ;---------------------------------------------- 
         subMenu = xTauSettings,    "&MAPdot Settings",               0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}    
         subMenu = XTrpmsdial,      "&RPM Values",                    0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}

   menuDialog = main
       menu = "Oth&er Tuning"
         subMenu = coldAdvance,     "&Cold Advance",                  0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_separator    ;----------------------------------------------
         subMenu = manifoldTempCorr,"I&AT-Based Fuel Correction",     0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = matBasedRetard,  "IAT-&Based Timing Retard",       0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_separator    ;----------------------------------------------	
         subMenu = iacSteps,        "I&dle Steps",                    0, { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
         subMenu = ipwBins,         "Idle &PWM Dutycycle",            0, { IdleCtl == 4 }	
         subMenu = std_separator    ;----------------------------------------------
         subMenu = alphaMAPMap,     "Alpha-&N MAP Table",             0, { algorithm > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)} 
         subMenu = std_separator    ;----------------------------------------------
         subMenu = MAFtable1,       "&MAF Correction Table",          0, { MAFOption > 0 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}

   menuDialog = main
      menu = "Tools"
         subMenu = std_ms2gentherm, "Calibrate T&hermistor Tables...",0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_ms2geno2,    "Calibrate &AFR Table...",        0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = mafTableBurner,  "Calibrate &MAF Table...",        0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}         
         subMenu = sensorCal,       "&Sensor Calibration...",         0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
         subMenu = std_trigwiz,     "Tri&gger Wizard...",             0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}
	 subMenu = injector_test,   "&Injector Test Mode",            0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}     
         subMenu = canOutmsgBurner,  "Configure &CAN outmsg...",      0,  { ECUType == 1 || ECUType == 2 || ECUType == 3}         

   menu = "Help"
#if MS2_SEQ
         subMenu = RFhelp,          "Req_Fuel Settings"
         subMenu = seqGeneral,      "Sequencer Info"
#else
         subMenu = helpGeneral,     "&MS-II Info"
#endif
         subMenu = sensorHelp,      "&Sensor Calibration"
         subMenu = burnHelp,        "&Burning Values to ECU"

;-------------------------------------------------------------------------------

[UserDefined]

   dialog = generalSettings, "General Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#sg"
      field = "ECU Type",                 ECUType
      field = "!MUST set ECU Type before editing other values."
      field = "#MS-II = 1"
      field = "#MicroSquirt = 2"
      field = "#Sequencer = 3"
;      field = "Sequencer Acknowledge",    seq_ack,             { ECUType == 3}
      field = "#"	  
      field = "Engine displacement",      CID,                 { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "Manifold displacement",    Vmfld,               { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "Compression Ratio",           CR,               { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "Injector Flow Rate",       fRate,
#if AUTO_TRIG      
       field = "Injection Timing Angle",   InjStart,            { ECUType == 2 || ECUType == 3}
;      field = "Spark/Fuel Offset",        spark_fuel_offset,   { !autoTrig && {ECUType == 2 || ECUType == 3}}
#else
       field = "Injection Timing Delay",   InjStart,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
       field = "!Spark/Fuel Offset",       spark_fuel_offset,   { ECUType == 2 || ECUType == 3}
#endif
;     field = "#System"
;     field = "Temperature Units",        tempUnits,           { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "Dual Table Use",           dualTable,           {flexFuel != 2 && (ECUType == 1 || ECUType == 2 || ECUType == 3)}
      field = "Barometric Correction",    baroCorr,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      #  set X_TAU_VISIBLE
      #if X_TAU_VISIBLE
      field = "X-Tau Usage",              xTauOption,          { ECUType == 1 || ECUType == 2 || ECUType == 3}
      #endif
      field = "Prime, CrankPW, & ASE Tables", CWOption,        { ECUType == 1 || ECUType == 2 || ECUType == 3}

   dialog = samplerate, "Sampling and Smoothing" 
      topicHelp = "http://www.megamanual.com/mt28.htm#ls"	  
      field = "#Input Smoothing Factors (%)"
      field = "MAP Averaging Lag Factor",    mapLF,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "MAF Averaging Lag Factor",    mafLF,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "RPM Averaging Lag Factor",    rpmLF,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "TPS Averaging Lag Factor",    tpsLF,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "Lambda Averaging Lag Factor", egoLF,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "CLT/IAT/Battery Lag Factor",  adcLF,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "Knock Averaging Lag Factor",  knkLF,            { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "#Sampling Rates"
      field = "TPSDOT Sample Rate",          tpsdotSample,     { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "MAP/MAFDOT Min Sample Rate",  airdotSample,     { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "#Sampling Points"
      field = "MAP Sample Point Rel TDCC1",   mapSample,       { ECUType == 1 || ECUType == 2 || ECUType == 3}
      field = "MAF Sample Point Rel TDCC1",   mafSample,       { ECUType == 1 || ECUType == 2 || ECUType == 3}

   dialog = revLimiter, "Rev Limiter"
      topicHelp = "http://www.megamanual.com/mt28.htm#sr"
      field = "Algorithm",                   RevLimOption
      field = "Maximum Retard",              RevLimMaxRtd,     { RevLimOption == 1 }
      field = "Lower Rev Limit",             RevLimRpm1
      field = "Upper Rev Limit",             RevLimRpm2

   dialog = flexFuelSettings, "Flex Fuel Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#sf"
      field = "Flex Fuel Sensor",           flexFuel
      field = "Frequency (low)",            fuelFreq0,         { flexFuel == 1 }
      field = "Fuel Correction (low)",      fuelCorr0,         { flexFuel == 1 }
      field = "Timing Correction (low)",    fuelSpkDel0,       { flexFuel == 1 }
      field = "Frequency (high)",           fuelFreq1,         { flexFuel == 1 }
      field = "Fuel Correction (high)",     fuelCorr1,         { flexFuel == 1 }
      field = "Timing Correction (high)",   fuelSpkDel1,       { flexFuel == 1 }

   dialog = can_activate, "Activate CAN Out Messages"
      field = "Enable Msg 0",             activate_xrate_0
      field = "Enable Msg 1",             activate_xrate_1
      field = "Enable Msg 2",             activate_xrate_2
      field = "Enable Msg 3",             activate_xrate_3
      field = "Enable Msg 4",             activate_xrate_4
      field = "Enable Msg 5",             activate_xrate_5
      field = "Enable Msg 6",             activate_xrate_6
      field = "Enable Msg 7",             activate_xrate_7
 
   dialog = otherFuel, "Other Fuel Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#lo"	  
      field = "#Engine Start Up"
      field = "Max. Cranking Speed",        crankingRPM,       { 1 }
      field = "TPS for Flood Clear Mode",   floodClear
      field = "#VE Table Adjustments"
      field = "(May have to save MSQ and reload to get to stick)"
      field = "VE/SPK/AFR table index",    VEIXOptn,         { 1 }
      field = "    - For MAP/Baro also set/unset MAPbaro in Properties -"
      field = "    - Must use PID43 for MAF only -"
      field = "Res Gas Model VE Calc",        VERGMOptn,         { MAFOption != 1}
      field = "Valve Overlap Factor",         VOF,               { VERGMOptn > 0 }
      field = "RGM Coeff 1 (Backflow)",      c1rgm,              { VERGMOptn > 0 }
      field = "RGM Coeff 1 (Trapped egr)",   c2rgm,              { VERGMOptn > 0 }
      field = "AFR Table Fuel Calc Usage",  AFRMult,           { 1 }
      field = "AFR Stoich. Ratio",          AFRStoich,         { 1 }
      field = "#Two-Point Prime"
      field = "Prime Pulse Cold PW",        primePulseCold,    { CWOption == 0 }
      field = "Prime Pulse Hot PW",         primePulseHot,     { CWOption == 0 }
      field = "Prime Delay", prime_delay

      field = "#Additional Fuel (switched by E0 low or cyclic)"
#if n2o
      field = "Nitrous Oxide Enrichment",   n2oEnrich
	  field = "Spark Retard When N2O Active", spkN2O
#else 
      field = "Fuel Added to Base PW",      pwImpulse
      field = "#Additional Fuel (cyclic only)"
      field = "Time Between Added Fuel",    impulseSec
      field = "Number of Cycles",           nImpulse
#endif
   
  dialog = aseSettings, "Start/ AfterStart Enrichment Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#ss"

      field = "#Cranking Pulsewidth"
#if MS2_SEQ
      field = "!Crank Pulses",            CPWOption,
#else
      field = "Crank Pulses",            CPWOption,
#endif
      field = "Cold Crank PW",            crankCold,          { CPWOption && CWOption == 0 }
      field = "Hot Crank PW",             crankHot,           { CPWOption && CWOption == 0 }
      field = "Tach Cycles per Squirt",   nskpCPW,            { ECUType == 3 && CPWOption == 2 }
#if MS2_SEQ
      field = "!Red settings require an MS-II reboot!"
#endif
    
      field = "#Hot AfterStart Enrichment"
      field = "ASE Hot Start Enable",    ASEHot

      field = "#Two-Point AfterStart Enrich"
      field = "ASE Cold Percent",        asePctCold,          { CWOption == 0 }
      field = "ASE Hot Percent",         asePctHot,           { CWOption == 0 }
      field = "ASE Cold Count",          aseCountCold,        { CWOption == 0 }
      field = "ASE Hot Count",           aseCountHot,         { CWOption == 0 }
  
  dialog = accSettings, "Accel Enrichment Configuration"
      topicHelp = "http://www.megamanual.com/mt28.htm#sl"
      field = "#AE RPM Scaling (for non-XTau accel)"
      field = "Low RPM Threshold",       ae_lorpm,
      field = "High RPM Threshold",      ae_hirpm,
  
   dialog = baroCorrection, "2-Point Barometric Correction"
      topicHelp = "http://www.megamanual.com/mt28.htm#sb"
      field = "#Barometric Correction"
      field =    "At total vacuum ",     bcor0
      field =    "Rate",                 bcormult

   dialog = xTauSettings, "X-Tau MAPdot Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#um"
      field = "#MAPdot Thresholds for transition to X, Tau Decel Tables"
      field = "Start Transition",  MapThreshXTD
      field = "Finish Transition",  MapThreshXTD2      
      field = "#"
      field = "#MAPdot trending threshhold is the start of"
      field = "#Map Trending for faster AE/ XTau enrichment"
      field = "MAPdot Trending Threshhold",        MapThreshXTA
      field = "Max. MAP added per sample",         trendmapLimit
	  
   dialog = injChars, "Injector Characteristics"
      topicHelp = "http://www.megamanual.com/mt28.htm#sn"
      field = "Injector Open Time",         injOpen
      field = "Battery Voltage Correction", battFac
      field = "PWM Current Limit",          injPwmP,     { ECUType == 1 }
      field = "PWM Time Threshold",         injPwmT,     { ECUType == 1 }
      field = "!Injector PWM Period",       injPwmPd,    { ECUType == 1 }
      field = "!Red settings require an MS-II reboot!"

   dialog = egoControl, "EGO Control"
      topicHelp = "http://www.megamanual.com/mt28.htm#se"
      field = "EGO Sensor Type",           egoType
      field = "NB Stoich Voltage",         NBVStoich,    { egoType == 1 || egoType == 2 || egoType == 5 }
      field = "AFR Stoich Ratio",          AFRStoich,    { egoType > 0 }
      field = "AFR Stoich for 2nd FlexFuel",  AFRStoichFF,    { egoType > 0 && flexFuel > 0}

      field = "Ignition Events per Step",  egoCount,     { (egoType == 1 || egoType == 2 || egoType == 5) || (egoType >  2  && egoAlgorithm == 0)}

      field = "Controller Step Size",      egoDelta,     { egoType == 1 || egoType == 2 || egoType == 5}
      field = "Controller Authority ±",    egoLimit,     { egoType >  0 }
      field = "Active Above Coolant Temp", egoTemp,      { egoType >  0 }
      field = "Active Above RPM",          egoRPM,       { egoType >  0 }
      field = "Active Below TPS",          TPSOXLimit,   { egoType >  0 }
      field = "Active Below MAP",          MAPOXLimit,   { egoType >  0 }

   field = "#WB Controller Settings"
      field = "Algorithm",                 egoAlgorithm, { egoType >  2 && egoType != 5}
      field = "PID Proportional Gain",     egoKP,        { egoType >  2 && egoType != 5 }
      field = "Transport Delay 1",         egoKdelay1,   { egoType >  2 && egoType != 5 && egoAlgorithm > 0 }
      field = "Transport Delay 2",         egoKdelay2,   { egoType >  2 && egoType != 5 && egoAlgorithm > 0 }
      field = "PID Integral",              egoKI,        { egoType >  2 && egoType != 5 && egoAlgorithm > 1 }
      field = "PID Derivative",            egoKD,        { egoType >  2 && egoType != 5 && egoAlgorithm > 1 }
      field = "#" 
      field = "#To stop Closed Loop but not sensor "
      field = "#readings, set 'Active Below MAP' to 0"

   dialog = amcSettings, "Automatic Mixture Control"
      topicHelp = "http://www.megamanual.com/mt28.htm#lm"
      field = "!Must have EGO correction enabled for AMC to operate!"
      field = "Automatic Mixture Control", AMCOption,    { egoType   > 0 }
      field = "Step size",                 AMCstep,      { AMCOption > 0 }
      field = "Minimum VE Change",         AMCdve,       { AMCOption > 0 }
      field = "Vertex Tolerance",          AMCve_rpm,    { AMCOption > 0 }
      field = "Vertex Tolerance",          AMCve_map,    { AMCOption > 0 }
      field = "Table Change Interval",     AMCramve_dt,  { AMCOption > 0 }
      field = "Flash Update Interval",     AMCT_thresh,  { AMCOption > 1 }
      field = "Update After",              AMCupdate_thresh, { AMCOption > 1 }
   
   dialog = alphaNOptions, "Alpha-N Blending"
      topicHelp = "http://www.megamanual.com/mt28.htm#la"
      field = "Low RPM Blend Threshold - AlphaN below",  alpha_lorpm
      field = "High RPM Blend Threshold - SD above",     alpha_hirpm
      field = "Invert above AlphaN/SD blend logic",      alphDir
      field = "Baro Spark Advance (deg/kPa below 100)",  alpha_baro_spkadv

   dialog = ignitionOptions, "Base Ignition Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#ib"
      field = "#General Ignition"
      field = "Trigger Offset",            triggerOffset
      field = "Skip Pulses",               no_skip_pulses
      field = "#Prediction Settings",      
      field = "Predictor Algorithm",       PredOpt
      field = "Alpha",                     alpha,           { PredOpt == 1 }
      field = "Beta",                      beta,            { PredOpt == 1 }
      field = "Gamma",                     gamma,           { PredOpt == 1 }
      field = "#Tach Signal Masking" 
      field = "Time Mask",                 ICISR_tmask
      field = "Percentage Mask",           ICISR_pmask
      field = "#Next-Pulse Tolerance"
      field = "   Cranking",               crankTolerance
      field = "   After-start",            asTolerance
      field = "   Normal Running",         pulseTolerance
      field = "Check Tach Sync Options",   acc_synchk,      { triggerTeeth == 0 }
      field = "!Ignition Input Capture",   ICIgnCapture,    { ICIgnOption != 2 && ICIgnOption != 3 } ; !
      field = "!Cranking Trigger",         ICCrankTrigger,  { ICIgnOption != 2 && ICIgnOption != 3 } ; !
      field = "!Coil Charging Scheme",     ICIgnOption  ; !
      field = "!Spark Output",             spkout_hi_lo,    { ECUType != 3 } ; !

   dialog = dualmultisparkoptions, "#Dual/Multi Spark Ignition Options"
      topicHelp = "http://www.megamanual.com/mt28.htm#ia"
      field = "!Dual/Multi Spark Options",      DualSpkOptn
      field = "!Auto Trigger Calculation",      autoTrig
      field = "!Offset (advance) for Output #2", OddAng
      field = "!Connect Outputs #1, 2",          tie1_2cyl,     { nCylinders == 1 && DualSpkOptn > 1 && DualSpkOptn != 6 || nCylinders == 2 && DualSpkOptn == 4 || DualSpkOptn >= 7 }
      field = "!Red settings require an MS-II reboot!"

   dialog = AdvncdignitionOptions, "Advanced Ignition Options"
      topicHelp = "http://www.megamanual.com/mt28.htm#ia"
      field = "#Trigger Wheel Only (0 is no trigger wheel)"
      field = "#Set only with ENGINE OFF"
      field = "!Trigger Wheel Teeth",          triggerTeeth
      field = "!Missing Teeth",                No_Miss_Teeth,  { triggerTeeth > 0 }
#if AUTO_TRIG
#else
      field = "!Skip Teeth",                   No_Skip_Teeth,  { triggerTeeth > 0 && !autoTrig}
      field = "Delay Teeth",                   Delay_Teeth,    { triggerTeeth > 0 && !autoTrig}
#endif
      field = "Cam Tooth",                     Cam_Tooth
      field = "#IAT-based Spark Retard Limiting Options"       
      field = "Start IAT Retard ",              MatRtdRPMLo
      field = "Full IAT Retard ",               MatRtdRPMHi
      field = "#Signal Delay Parameters"
      field = "FET Ouput Delay",                fet_delay
      field = "VR Input Delay",                 vr_delay     
      field = "!Red settings require an MS-II reboot!"

   dialog = dwellSettings, "Dwell Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#iw"
      field = "Maximum Dwell Duration",        max_coil_dur
      field = "Maximum Spark Duration",        max_spk_dur
      field = "Acceleration Compensation",     dwellAcc
      field = "#Battery Voltage Compensation"
      ; Make this an array2D when available.
      array1D   = "", "Voltage  %INDEX% ", dwellVolts
      array1D   = "", "Duration at Voltage %INDEX% ", dwellDuration

   dialog = tachSettings, "Tach Signal Settings"
;      topicHelp = "http://www.megamanual.com/mt28.htm#??"
      field = "#Generally select one, zero other"
      field = "TachOut Fixed PW",        tachoPW
      field = "Tachout Duty Cycle",      tachoDuty

   dialog = idleControl, "Idle Control"
      topicHelp = "http://www.megamanual.com/mt28.htm#sd"
      field = "Algorithm",                     IdleCtl
      field = "Fast Idle Temperature",         fastIdleT,    { IdleCtl == 1 }
      field = "Time Step Size",                IACtstep,     { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 }
      field = "Acceleration Step Size",        IACaccstep,   { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 }
      field = "Minimum # steps to move",       IACminstep,   { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 }
      field = "!PWM Frequency",                IACpwm_step,  { IdleCtl == 4 }
      field = "!Start Value (retract)",        IACStart,     { IdleCtl > 1 } ; !
      field = "Cranking Position (extend)",    IACcrankpos,  { IdleCtl > 1 }
      field = "Crank-to-Run Taper Time",       IACcrankxt,   { IdleCtl > 1 }
      field = "Hysteresis",                    IdleHyst,     { IdleCtl >= 1 }
      field = "#Time-Based After Start (extended warm-up)"
      field = "   Cold Temperature",           IACcoldtmp,   { IdleCtl > 1 }
      field = "   Cold Position",              IACcoldpos,   { IdleCtl > 1 }
      field = "   Cold Taper Time",            IACcoldxt,    { IdleCtl > 1 }

   dialog = sensorCal, "Sensor Calibration"
      topicHelp = sensorHelp
      field = "#MAP Sensor (F1 for common values)"
      field =    "Value at 0.0 volts",   map0
      field =    "Value at 5.0 volts",   mapmax
      field = "#Barometer Sensor (usually identical to MAP)"
      field =    "Value at 0.0 volts",   baro0
      field =    "Value at 5.0 volts",   baromax

   dialog = knockSettings, "Knock Sensor Settings"
      topicHelp = "http://www.megamanual.com/mt28.htm#ik"
      field = "Knock Control",        knkOption
      field = "#Detection"
      field = "Threshold Direction",  knkDirection,     { knkOption > 0 }
      field = "knock value at 0V",    knock0
      field = "knock value at 5V",    knockmax
      field = "Knock Count",          knk_ndet,         { knkOption > 0 }
      field = "No Knock Above MAP",   knk_maxmap,       { knkOption > 0 }
      field = "No Knock Below RPM",   knk_lorpm,        { knkOption > 0 }
      field = "No Knock Above RPM",   knk_hirpm,        { knkOption > 0 }
      field = "#Retarding"
      field = "Maximum Retard",       knk_maxrtd,       { knkOption > 0 }
      field = "Retard Check Time",    knk_trtd,         { knkOption > 0 }
      field = "Retard Step Size",     knk_step1,        { knkOption > 0 }
      field = "#Recovery"
      field = "Advance Check Time",   knk_tadv,         { knkOption > 0 }
      field = "Advance Step Size",    knk_step2,        { knkOption > 0 }
      field = "Recovery Advance",     knk_dtble_adv,    { knkOption > 1 }

   dialog = injector_test, "Injector Test Mode"
      topicHelp = "http://www.megamanual.com/mt28.htm#oi"
      field = "!Injector test mode",  injTestMode ; !
      field = "Injector test squirts",  injTestSqrts,    { injTestMode > 0 }
      field = "Injector test PW",  injTestPW,            { injTestMode > 0 }
      field = "Injector test offtime",  injTestOffTime,  { injTestMode > 0 }
      field = "!Reboot to test, set to 'Normal Mode' to reset"

   dialog = frpmTableBins, "RPM Table Bins for Fuel Tables"
      topicHelp="http://www.megamanual.com/mt28.htm#"
      array1D   = "", "Fuel RPM  %INDEX% ", frpm_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = fmapTableBins, "MAP Table Bins for Fuel Table(s)"
      topicHelp="http://www.megamanual.com/mt28.htm#"
      array1D   = "", "Fuel MAP  %INDEX% ", fmap_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = srpmTableBins, "RPM Table Bins for Spark Table"
      topicHelp="http://www.megamanual.com/mt28.htm#"
      array1D   = "", "Spark RPM  %INDEX% ", srpm_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = smapTableBins, "MAP Table Bins for Spark Table"
      topicHelp="http://www.megamanual.com/mt28.htm#"
      array1D   = "", "Spark MAP  %INDEX% ", smap_table
      field = "#Close and re-open Table(s) to see changes"

   dialog = tempTableBins, "Temperature Table Values"
      topicHelp="http://www.megamanual.com/mt28.htm#at"
      array1D   = "", "Temperature  %INDEX% ", tempTable
      
    dialog = XtempTableBins, "X Temperature Correction Values"
      topicHelp="http://www.megamanual.com/mt28.htm#at"
      field = "#Temperature Correction for X Enrichments"
      array1D   = "", "Correction  %INDEX% ", XClt
  
      dialog = TtempTableBins, "Tau Temperature Correction Values"
      topicHelp="http://www.megamanual.com/mt28.htm#at"
      array1D   = "", "Correction  %INDEX% ", TauClt
 
   dialog = XTrpmsdial, "X-Tau RPM Values"
      topicHelp="http://www.megamanual.com/mt28.htm#ur"
      field = "#RPM Bins for X-Tau Enrichments"                                                    
      array1D   = "", "X-Tau RPM  %INDEX% ", XTrpms

   dialog = fueltrim, "Individual Cylinder Fuel Trim (%)"
      topicHelp="http://www.megamanual.com/mt31.htm#yf"                                               
      array1D   = "", "Cylinder  %INDEX% ", ftrim

   dialog = sparktrim, "Individual Cylinder Spark Trim (degrees)"
      topicHelp="http://www.megamanual.com/mt31.htm#ys"                                               
      array1D   = "", "Cylinder  %INDEX% ", strim

   dialog = MAFSettings, "MAF vrs. MAP Usage"
      topicHelp = "http://www.megamanual.com/mt28.htm#lu"
      field = "#See Tables for MAF flow setting"
      field = "Enable MAF Use",             MAFOption
      field = "MAF Pin Configuration", MAFpin,   { MAFOption > 0 }
      field = "MAF Type Configuration", MAFtype, { MAFOption > 0 }
      field = "Note: MAF must NOT be on MAP pin for MAF + MAP."
      field = "Note: MAF MUST be on Knock pin for Freq MAF."
      field = "!Note: MUST reboot to enable changes to above!"
      field = "#MAP MAF Blend Settings"
      field = "MAP Only Below RPM",         MAFRPM1,  { MAFOption == 2 }
      field = "MAF Only Above RPM",         MAFRPM2,  { MAFOption == 2 }
      field = "Invert above MAP/MAF settings",       MAFDir,  { MAFOption == 2 }
      field = "MAF FF Time Lag",           maf_tlag,  { MAFOption > 2 }

      field = "#Viewing MAF in Real Time"
      field = "You can set one of the gauges on the front page to mafGauge"
      field = "to see the MAF in real time. Right click on any gauge and"
      field = "select mafGuage "
	  
   help = burnHelp, "Burning Values to ECU"
      webHelp = "http://www.megamanual.com/mt28.htm"
      text = "Occassionally, you may have trouble getting values to 'stick'"
      text = "in MegaTune. There are a few things you can try if this happens:<br><br>"
      text = "\tHit TAB after entering the value. This forces MegaTune to" 
      text = "recognize the changed value.<br>" 
      text = "\tThen 'Burn to ECU'<br><br>"	
      text = "If that doesn't work:<br><br>"	
      text = "\tChange the value (as above) and immediately save the MSQ file ('File/Save').<br>"
      text = "\tThen reload the file you just saved, and burn it when prompted.<br><br>"
      text = "This forces all the values to be burned to both flash and RAM memory, and"
      text = "should solve the problem."	
 	  
   help = sensorHelp, "Sensor Calibration"
      webHelp = "http://www.megamanual.com/mt28.htm#os"
      text = "MAP Sensor Calibration<br>"
      text = "<br>"
      text = "For the\tMPX4115   use\t10.6 and \t121.7<br>"
      text = "\tMPX4250\t\t10.0\t260.0<br>"
      text = "\tMPXH6300\t1.1\t315.5<br>"
      text = "\tGM 3-BAR\t1.1\t315.5<br>"
      text = "\tMPXH6400\t3.5\t416.5<br>"
      text = "<br>"
      text = "(GM 3-bar data from Dave Hartnell, http://www.not2fast.com/electronics/component_docs/MAP_12223861.pdf)<br>"
      text = "<br>"
      text = "\tSensor type\tvLo\tpLo\tvHi\tpHi\tvRef<br>"
      text = "\tMPX4115 \t0.204 v\t15 kPa\t4.794 v\t115 kPa\t5.100 v<br>"
      text = "\tMPX4250 \t0.204 v\t20 kPa\t4.896 v\t250 kPa\t5.100 v<br>"
      text = "\tMPXH6300\t0.306 v\t20 kPa\t4.913 v\t304 kPa\t5.100 v<br>"
      text = "\tGM 3-BAR\t0.631 v\t40 kPa\t4.914 v\t304 kPa\t5.100 v<br>"
      text = "\tMPXH6400\t0.200 v\t20 kPa\t4.800 v\t400 kPa\t5.000 v<br>"
      text = "<br>"
      text = "In general, use values derived from these equations:<br>"
      text = "<br>"
      text = "\tm = (pHi-pLo)/(vHi-vLo)<br>"
      text = "\tpv1 = pLo - m * vLo<br>"
      text = "\tpv2 = pv1 + m * vRef<br>"
      text = "<br>"
      text = "References:<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPX4115A.pdf<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPX4250A.pdf<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPXH6300A.pdf<br>"
      text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPXH6400A.pdf<br>"
      text = "<br>"
      text = "Barometer Sensor Calibration<br>"
      text = "<br>"
      text = "If your system has an external barometer sensor, separate from the MAP"
      text = "sensor, then use these values to calibrate it properly.  If you have"
      text = "a standard MS installation, then copy your MAP sensor values here.<br>"
      text = "<br>"
      text = "Barometric Correction Calibration<br>"
      text = "<br>"
      text = "Correction for barometric effects is performed using the linear function below.<br>"
      text = "<br>"
      text = "\tcorrection = correction_0 + (rate * barometer) / 100<br>"
      text = "<br>"
      text = "'At total vacuum' contains the total correction at a barometer reading"
      text = "of 0 kPa (you are on the moon).  The 'Rate' contains the percentage per 100"
      text = "kPa to scale the barometer value.  Using the default values of 147 and -47,"
      text = "we see that for a barometer of 100 kPa, we have 100% correction.<br>"
      text = "<br>"
      text = "\tcorrection = 147 + (-47*100) / 100 = 100%"

   help = RFhelp, "Req_Fuel Help"
      webHelp = "http://www.megamanual.com/seq/"
      text = "To make the ReqFuel and duty cycle values correct"
      text = "it is necessary to set the following parameters:<br>"
      text = "\tinjections per engine cycle = number of cylinders<br>"
      text = "\tinjector staging = Simultaneous<br>"
      text = "\tengine stroke = 4-stroke (2-stroke not yet tested)<br>"
      text = "\tinjection port type = Port Injection<br>"
      text = "\tNumber of injectors = 1 regardless of actual number<br>"
      text = "<br>"
      text = "In addition, the #set MS_SEQ  line must be in the"
      text = "settings.ini file."

   help = helpGeneral, "MS-II General Info"
      webHelp = "http://www.megamanual.com/mt28.htm"
      text = "Al Grippo and Bruce Bowling have created MegaSquirt-II, which"
      text = "is a plug-in daughter card that replaces the 8-bit MC68HC908GP32"
      text = "with a 16-bit MC9S12C64 processor."
      text = "<br>"
      text = "It is basically a plug-in processor card that has the MC9S12C64"
      text = "processor plus support hardware as well as a stepper motor chip,"
      text = "and an ignition module controller.  The embedded code is written"
      text = "in C, rather than assembly language, so it should be more accessible"
      text = "to more programmers (Stephane Carrez has ported GCC to the HC12"
      text = "processor so, although it doesn't use the full 9S12 instruction"
      text = "set, we are able to use his version to write code for the MS-II).<br>"
      text = "<br>"
      text = "For current documentation, click the Web Help button below, or for"
      text = "support questions visit http://www.msefi.com/."

   help = seqGeneral, "MS-II Sequencer Info"
      webHelp = "http://www.megamanual.com/seq/"
      text = "Al Grippo and Bruce Bowling have created the MS-II Sequencer"
      text = "EFI controller, which is purchased fully assembled.<br>"
      text = "The MS-II Sequencer has two 16-bit MC9S12C64 processors.<br>"
      text = "The MS-II Sequencer can provide sequential fuel and"
      text = "ignition control for up to 8 injectors/COP with crank"
      text = "wheel and cam signals<br>"  
      text = "For current documentation, click the Web Help button below, or for"
      text = "support questions visit http://www.microsquirt.com/."  

;-------------------------------------------------------------------------------

[CurveEditor]
   curve = coldAdvance, "Cold Ignition Advance Offset"
      topicHelp   = "http://www.megamanual.com/mt28.htm#ec"
      columnLabel = "Coolant", "Offset"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif 
      yAxis       = -10,  10, 5
      xBins       = tempTable, coolant
      yBins       = cold_adv_table
      gauge       = cltGauge

   curve = iacSteps, "IAC Steps"
      topicHelp   = "http://www.megamanual.com/mt28.htm#ed"
      columnLabel = "Coolant", "IAC Steps"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 300, 7
      xBins       = tempTable, coolant
      yBins       = iacstepTable
      gauge       = cltGauge

   curve = ipwBins, "PWM Idle Duty Cycle"
      topicHelp   = "http://www.megamanual.com/mt28.htm#ep"
      columnLabel = "Coolant", "Idle PWM"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 100, 6
      xBins       = tempTable, coolant
      yBins       = ipwmTable
      gauge       = cltGauge

   curve = primingPW, "Priming Pulsewidth"
     topicHelp   = "http://www.megamanual.com/mt28.htm#rm"
      columnLabel = "Coolant", "Prime PW"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0,  20, 5
      xBins       = tempTable, coolant
      yBins       = primePWTable
      gauge       = cltGauge

   curve = crankingPW, "Cranking Pulsewidth"
     topicHelp   = "http://www.megamanual.com/mt28.htm#rn"
      columnLabel = "Coolant", "Cranking PW"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0,  20, 5
      xBins       = tempTable, coolant
      yBins       = crankPWTable
      gauge       = cltGauge

   curve = asePct, "Afterstart Enrichment Percentage"
     topicHelp   = "http://www.megamanual.com/mt28.htm#rs"
      columnLabel = "Coolant", "Afterstart"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 100, 6
      xBins       = tempTable, coolant
      yBins       = asePctTable
      gauge       = cltGauge

   curve = aseTaper, "Afterstart Enrichment Taper"
     topicHelp   = "http://www.megamanual.com/mt28.htm#re"
      columnLabel = "Coolant", "Taper"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =   0, 500, 6
      xBins       = tempTable, coolant
      yBins       = aseCntTable
      gauge       = cltGauge

   curve = matBasedRetard, "IAT-Based Spark Timing Retard"
     topicHelp   = "http://www.megamanual.com/mt28.htm#eb"
      columnLabel = "IAT", "Retard"
      xAxis       = 100, 300, 9
      yAxis       =   0,  15, 7
      xBins       = matTemps, mat
      yBins       = matRetard
      gauge       = matGauge

   curve = knockThresholdCurve, "Knock Threshold"
     topicHelp   = "http://www.megamanual.com/mt28.htm#ik"
      columnLabel = "RPM", "Threshold"
      xAxis       =   0, 6000, 7
      yAxis       =   0,  5.0, 6
      xBins       = knk_rpm, rpm
      yBins       = knk_thresh
      gauge       = tachometer

   curve = barometerCorr, "Non-Linear Barometric Correction"
     topicHelp   = "http://www.megamanual.com/mt28.htm#rc"
      columnLabel = "Barometer", "Correction"
      xAxis       =  60, 120, 7
      yAxis       = -30,  30, 7
      xBins       = baroCorrVals, barometer
      yBins       = baroCorrDelta
      gauge       = barometerGauge

   curve = manifoldTempCorr, "Non-Linear IAT (intake air temperature) Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt28.htm#ea"
      columnLabel = "IAT", "Correction"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =  -30,  30, 7
      xBins       = matCorrTemps, mat
      yBins       = matCorrDelta
      gauge       = matGauge
   
   curve = XAccTable, "X Accel Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt28.htm#ua"
      columnLabel = "RPM", "Correction"
      xAxis       =    0,  8000, 4
      yAxis       =    0,   120, 4
      xBins       = XTrpms, rpm
      yBins       = XAccTable
      gauge       = xTauGauge1
        
   curve = XDecTable, "X Decel Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt28.htm#ud"
      columnLabel = "RPM", "Correction"
      xAxis       =    0,  8000, 9
      yAxis       =    0,   120, 9
      xBins       = XTrpms, rpm
      yBins       = XDecTable
      gauge       = xTauGauge1
       
   curve = TauAccTable, "Tau Accel Fuel Correction"
     topicHelp   = "http://www.megamanual.com/mt28.htm#uc"
      columnLabel = "RPM", "time"
      xAxis       =    0,  8000, 9
      yAxis       =    0,  1000, 9
      xBins       = XTrpms, rpm
      yBins       = TauAccTable
      gauge       = xTauGauge1
 
   curve = TauDecTable, "Tau Decel Correction"
     topicHelp   = "http://www.megamanual.com/mt28.htm#ue"
      columnLabel = "RPM", "time"
      xAxis       =    0,  8000, 9
      yAxis       =    0,  1000, 9
      xBins       = XTrpms, rpm
      yBins       = TauDecTable
      gauge       = xTauGauge1 
      
   curve = XCltTable, "X (Puddling) Temp. Correction Factors"
     topicHelp   = "http://www.megamanual.com/mt28.htm#ux"
      columnLabel = "Temperature", "Correction"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =    0,   600, 9
      xBins       = tempTable
      yBins       = XClt
      gauge       = cltGauge 
      
   curve = TCltTable, "Tau (Time) Temp. Correction Factors"
     topicHelp   = "http://www.megamanual.com/mt28.htm#ut"
      columnLabel = "Temperature", "time"
    #if EXPANDED_CLT_TEMP 
      xAxis       = -40, 600, 9
    #else 
      xAxis       = -40, 250, 9
    #endif
      yAxis       =    0,   600, 9
      xBins       = tempTable
      yBins       = TauClt
      gauge       = cltGauge                 

	  
   curve = MAFtable1, "MAF Correction Table (to alter default MAF curve)"
     topicHelp   = "http://www.megamanual.com/mt28.htm#em"
      columnLabel = "MAF Flow", "Correction"
      xAxis       =  0, 300, 11
      yAxis       =  0, 255, 11
      xBins       = MAFFlow, maf
      yBins       = MAFCor
      gauge       = mafGauge
	  
	  
[TableEditor]

#if MAPbaro

   table = veTable1Tbl, veTable1Map, "VE Table 1 (MAP/baro)", 2
     topicHelp   = "http://www.megamanual.com/mt28.htm#a1"
      ;             constant,   variable
      xBins       = frpm_table, rpm,   readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable1

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340 ; Space 123 rotation of grid in degrees.

   table = veTable2Tbl, veTable2Map, "VE Table 2", 2
     topicHelp   = "http://www.megamanual.com/mt28.htm#a1"
      xBins       = frpm_table, rpm,   readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable2

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340


#else

   ;       table_id,    map3d_id,    "title",      page
   table = veTable1Tbl, veTable1Map, "VE Table 1 (MAP)", 2
     topicHelp   = "http://www.megamanual.com/mt28.htm#a1"
      ;             constant,   variable
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable1

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340 ; Space 123 rotation of grid in degrees.


   table = veTable2Tbl, veTable2Map, "VE Table 2", 2
     topicHelp   = "http://www.megamanual.com/mt28.htm#a1"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = veTable2

      upDownLabel = "RICHER", "LEANER"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340

#endif

#if LAMBDA
   table = afrTable1Tbl, afrTable1Map, "Lambda Table 1", 1
      gridHeight  = 3.0
#else
   table = afrTable1Tbl, afrTable1Map, "AFR Table 1", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt28.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = afrTable1
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

#if LAMBDA
   table = afrTable1Tblix, afrTable1MapIX, "Lambda Table 1", 1
      gridHeight  = 3.0
#else
   table = afrTable1Tblix, afrTable1MapIX, "AFR Table 1", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt28.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix,   readonly
      zBins       = afrTable1
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

#if LAMBDA
   table = afrTable2Tbl, afrTable2Map, "Lambda Table 2", 1
      gridHeight  = 3.0
#else
   table = afrTable2Tbl, afrTable2Map, "AFR Table 2", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt28.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix, readonly
      zBins       = afrTable2
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

#if LAMBDA
   table = afrTable2Tblix, afrTable2MapIX, "Lambda Table 2", 1
      gridHeight  = 3.0
#else
   table = afrTable2Tblix, afrTable2MapIX, "AFR Table 2", 1
      gridHeight  = 1.0
#endif
     topicHelp   = "http://www.megamanual.com/mt28.htm#af"
      xBins       = frpm_table, rpm,     readonly
      yBins       = fmap_table, kpaix,   readonly
      zBins       = afrTable2
      upDownLabel = "LEANER", "RICHER"
      gridOrient  = 250,   0, 340

   table = ignitionTbl, ignitionMap, "Spark Advance Table", 2
     topicHelp   = "http://www.megamanual.com/mt28.htm#ap"
      xBins       = srpm_table, rpm, readonly
      yBins       = smap_table, kpaix, readonly
      zBins       = advanceTable
      upDownLabel = "ADVANCING", "RETARDING"
      gridHeight  = 3.0
      gridOrient  = 250,   0, 340

   table = alphaMAPTbl, alphaMAPMap, "Alpha-N MAP Table", 1
     topicHelp   = "http://www.megamanual.com/mt28.htm#en"
      xBins       = amap_rpm, rpm
      yBins       = amap_tps, tps
      zBins       = alphaMAPtable
      upDownLabel = "UP", "DOWN"
      gridHeight  = 2.0
      gridOrient  = 250,   0, 340


;-------------------------------------------------------------------------------

[GaugeConfigurations]

   ;-------------------------------------------------------------------------------
   ;  Notes on some of the gauges.
   ;
   ;  The accelEnrichGauge is now a composite of both acceleration enrichment
   ;  and deceleration enleanment numbers.  See the definition of the variable
   ;  accDecEnrich in the OutputChannels section.
   ;
   ;  David Hooke contributed the lambda gauge and associated transfer
   ;  function files.
   ;
   ;  The lambda gauge is the best way (my opinion) to report data from a
   ;  wide band EGO gauge, it standardizes the output irrespective of fuel
   ;  or mix of fuels, so you needn't do any brainwork to know if your 75%
   ;  gasoline and 25% methanol is rich at 10:1 or not.
   ;
   ;  Use the file WBlambda100AVR.inc, if using a standard ADC (e.g., AVR cpu).
   ;  Use the file WBlambda100MOT.inc, if using a biased ADC (e.g., MOT cpu).
   ;-------------------------------------------------------------------------------
   ; Define a gauge's characteristics here, then go to a specific layout
   ; block (Tuning or FrontPage) and use the name you've defined here to
   ; display that gauge in a particular position.
   ;
   ; Name  = Case-sensitive, user-defined name for this gauge configuration.
   ; Var   = Case-sensitive name of variable to be displayed, see the
   ;         OutputChannels block in this file for possible values.
   ; Title = Title displayed at the top of the gauge.
   ; Units = Units displayed below value on gauge.
   ; Lo    = Lower scale limit of gauge.
   ; Hi    = Upper scale limit of gauge.
   ; LoD   = Lower limit at which danger color is used for gauge background.
   ; LoW   = Lower limit at which warning color is used.
   ; HiW   = Upper limit at which warning color is used.
   ; HiD   = Upper limit at which danger color is used.
   ; vd    = Decimal places in displayed value
   ; ld    = Label decimal places for display of Lo and Hi, above.

   ;Name               Var            Title                 Units     Lo     Hi     LoD    LoW   HiW   HiD vd ld

   advBucketGauge    = veTuneValue,   "Advance Bucket",     "degrees", 0,    55,    -1,     -1,  999,  999, 1, 1
   advdegGauge       = advance,       "Ignition Advance",   "degrees", 5,    50,    -1,     -1,  999,  999, 1, 1

   IACgauge          = iacstep,       "IAC position",       "steps",   0,   255,    -1,     -1,  999,  999, 0, 0
   dwellGauge        = dwell,         "Dwell",              "mSec",    0,    10,   0.5,    1.0,  6.0,  8.0, 1, 1
;  IAC step == idle pwm, when using pwm idle control.
   PWMIdlegauge      = idleDC,        "Idle PWM%",          "%",       0,   100,    -1,     -1,  999,   90, 0, 0

   accelEnrichGauge  = accDecEnrich,  "Accel Enrich",       "%",       0,   300,   -999,  -999,  999,  999, 0, 0
   accelEnrichPcnt   = accEnrichPcnt, "Accel Enrich",       "%",      50,   150,     -1,    -1,  999,  999, 0, 0
   accelEnrichMS     = accEnrichMS,   "Accel Enrich",    "msec",       0,  25.5,     -1,    -1,  999,  999, 1, 1
   decelEnrichPcnt   = decEnrichPcnt, "Decel Enrich",       "%",      50,   150,     -1,    -1,  999,  999, 0, 0
   decelEnrichMS     = decEnrichMS,   "Decel Enrich",    "msec",   -25.5,   0.0,    -25,   -25,    1,    1, 1, 1

   afr1Gauge         = afr1,          "Air:Fuel Ratio",     "",       10,  19.4,     12,    13,   15,   16, 2, 2
   afr2Gauge         = afr2,          "Air:Fuel Ratio 2",   "",       10,  19.4,     12,    13,   15,   16, 2, 2
   #if NARROW_BAND_EGO
     afrtgt1Gauge    = afrtgt1,       "Target EGO (V)",     "",       0,    1.0,     .2,    .3,   .6,   .8, 2, 2
     afrtgt2Gauge    = afrtgt2,       "Target EGO2 (V)",    "",       0,    1.0,     .2,    .3,   .6,   .8, 2, 2
   #elif LAMBDA
     afrtgt1Gauge    = afrtgt1,       "Target EGO (Lmbda)",     "",       0,    2.0,     .5,    .7,  1.3,  1.5, 2, 2
     afrtgt2Gauge    = afrtgt2,       "Target EGO2 (Lmbda)",    "",       0,    2.0,     .5,    .7,  1.3,  1.5, 2, 2
   #else
     afrtgt1Gauge    = afrtgt1,       "Target AFR",         "",       10,  19.4,     12,    13,   15,   16, 1, 1
     afrtgt2Gauge    = afrtgt2,       "Target AFR2",       "",       10,  19.4,     12,    13,   15,   16, 1, 1
   #endif
   clockGauge        = seconds,       "Clock",              "Seconds", 0,   255,     10,    10,  245,  245, 0, 0
   deadGauge         = deadValue,     "---",                "",        0,     1,     -1,    -1,    2,    2, 0, 0
   dutyCycle1Gauge   = dutyCycle1,    "Duty Cycle 1",       "%",       0,   100,     -1,    -1,   85,   90, 1, 1
   dutyCycle2Gauge   = dutyCycle2,    "Duty Cycle 2",       "%",       0,   100,     -1,    -1,   85,   90, 1, 1
   egoCorrGauge      = egoCorrection, "EGO Correction",     "%",      50,   150,     90,    99,  101,  110, 0, 0
   egoCorrGauge1     = egoCorrection1,"EGO Correction 1",   "%",      50,   150,     90,    99,  101,  110, 0, 0
   egoCorrGauge2     = egoCorrection2,"EGO Correction 2",   "%",      50,   150,     90,    99,  101,  110, 0, 0
   egoGauge          = egoVoltage,    "Exhaust Gas Oxygen", "volts",   0,   1.0,    0.2,   0.3,  0.7,  0.8, 2, 2
   ego2Gauge         = egoVoltage2,   "Exhaust Gas Oxygen2","volts",   0,   1.0,    0.2,   0.3,  0.7,  0.8, 2, 2
   engine            = engine,        "Engine Codes",       "",        0,   127,      0,     0,  127, 127,  0, 0  
   kpaixGauge        = kpaix,         "Table Load Index",    "kPa",     0,   255,      0,    20,  200,  245, 1, 0
   knockGauge        = knockRetard,   "Knock Retard",       "deg",     0,  25.0,     -1,    -1,  5.0, 10.0, 1, 1
   knockVGauge       = knock,         "Knock Volts",        "volts",   0,   5.0,     -1,    -1,  4.0, 5.0,  1, 1
   lambda1Gauge      = lambda1,       "Lambda",             "",      0.5,   1.5,    0.5,   0.7,    2,  1.1, 2, 2
   lambda2Gauge      = lambda2,       "Lambda",             "",      0.5,   1.5,    0.5,   0.7,    2,  1.1, 2, 2

   gammaEnrichGauge  = gammaEnrich,   "Gamma Enrichment",   "%",      50,   150,     -1,    -1,  151,  151, 0, 0
   mapGauge          = map,           "Engine MAP",         "kPa",     0,   255,      0,    20,  200,  245, 1, 0
   
   mafRaw            = mafraw,        "Raw MAF Sensor",      "g/sec",   0,   650,      0,   200,  480,  550, 2, 0
   mafSensor         = mafsensor,     "Corr. MAF Sensor",    "g/sec",   0,   650,      0,   200,  480,  550, 2, 0
   mafGauge          = maf,           "MAF Cyl Air flow",    "g/sec",   0,   650,      0,   200,  480,  550, 2, 0
   mafDOTGauge       = mafDOT,        "MAFDOT",             "g/sec^^2",  -600, 600,   -480, -200,  200, 550, 0, 0   
   mapmafGauge       = mapmaf,        "MAF from MAP",        "g/sec",   0,   650,      0,   200,  480,  550, 1, 0
   mafmapGauge       = mafmap,        "MAP from MAF",        "kPa",     0,   255,      0,    20,  200,  245, 1, 0
   mapDOTGauge       = mapDOT,        "MAPDOT",             "kPa/sec",  -600, 600,    -480, -200,  200, 550, 0, 0   
   barometerGauge    = barometer,     "Barometer",          "kPa",    60,   120,      0,    20,  200,  245, 1, 0
   calcMapGauge      = kpa,           "calcMAP",            "kPa",     0,   255,      0,    20,  200,  245, 1, 0
   pulseWidth1Gauge  = pulseWidth1,   "Pulse Width 1",      "mSec",    0,  25.5,    1.0,   1.2,   20,   25, 3, 1
   pulseWidth2Gauge  = pulseWidth2,   "Pulse Width 2",      "mSec",    0,  25.5,    1.0,   1.2,   20,   25, 3, 1
   tachometer        = rpm,           "Engine Speed",       "RPM",     0,  8000,    300,   500, 5000, 6000, 0, 0
   throttleGauge     = throttle,      "Throttle Position",  "%",       0,   100,     -1,     1,   90,  100, 0, 0
;   timmingErrGauge   = timingErr,     "Timing Error",       "degrees",-10,   10,    -10,    -5,    5,   10, 1, 1 
   deltaTGauge       = deltaT,        "Timing Delta",       "uS",      0, 25000,      0,     0,25000, 25000, 0, 0 
   veBucketGauge     = veTuneValue,   "VE Value",           "%",       0,   120,     -1,    -1,  999,  999, 0, 0
   veGauge           = veCurr1,       "VE Current",         "%",       0,   120,     -1,    -1,  999,  999, 0, 0
   veRGM             = vergm,         "VE Res Gas Model",   "%",       0,   120,     -1,    -1,  999,  999, 0, 0
   veMafMap          = vemafmap,      "VE from maf + map",  "%",       0,   120,     -1,    -1,  999,  999, 0, 0
   voltMeter         = batteryVoltage, "Battery Voltage",    "volts",   7,    21,     9,    10,   16,   17, 2, 2
   warmupEnrichGauge = warmupEnrich,  "Warmup Enrichment",  "%",     100,   150,     -1,    -1,  101,  105, 0, 0
   spare1Gauge       = spare1,        "spare1[0] spk_deg_err",     "",      -30,  30,    -10,  -5, 5,   10, 1, 1
   spare2Gauge       = spare2,        "spare2[1] reset count",     "",       0,  100,       0,    0,  32535,   17, 2, 2
   spare4Gauge       = spare4,        "spare4[3] count",        "",       0,  32535,     0,    0,  32535,   17, 2, 2
   spare5Gauge       = spare5,        "spare5[4] count",        "",       0,  32535,     0,    0,  32535,   17, 2, 2
   spare6Gauge       = spare6,        "spare6[5] count",        "",       0,  32535,     0,    0,  32535,   17, 2, 2
   spare7Gauge       = spare7,        "spare7[6] count",        "",       0,  32535,     0,    0,  32535,   17, 2, 2
   spare8Gauge       = spare8,        "spare8[7] count",        "",       0,  32535,     0,    0,  32535,   17, 2, 2
   spare9Gauge       = spare9,        "spare9[8] count",        "",       0,  32535,     0,    0,  32535,   17, 2, 2
 
 ;  Name               Var            Title                 Units     Lo     Hi     LoD    LoW   HiW   HiD vd ld
   xTauGauge1        = xTauFuelCorr1, "X-Tau Correction1",   "%",       0,   200,     40,    70,  130,  160, 0, 0
   xTauGauge2        = xTauFuelCorr2, "X-Tau Correction2",   "%",       0,   200,     40,    70,  130,  160, 0, 0

#if CELSIUS
  #if EXPANDED_CLT_TEMP
   cltGauge          = coolant,       "Coolant Temp",       "C",     -40,   600,     65,    93,  162,  176, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "C",     -40,   110,    -15,     0,   95,  100, 0, 0
  #else
   cltGauge          = coolant,       "Coolant Temp",       "C",     -40,   120,    -15,     0,   95,  105, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "C",     -40,   110,    -15,     0,   95,  100, 0, 0
  #endif
#else
  #if EXPANDED_CLT_TEMP
   cltGauge          = coolant,       "Coolant Temp",       "°F",    -40,   600,    150,   200,  325,  350, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "°F",    -40,   215,      0,    30,  200,  210, 0, 0
  #else
   cltGauge          = coolant,       "Coolant Temp",       "°F",    -40,   250,      0,    30,  200,  220, 0, 0
   matGauge          = mat,           "Intake Air Temp",    "°F",    -40,   215,      0,    30,  200,  210, 0, 0
  #endif
#endif

   e85Gauge          = fuelCorrection,"E85 Fuel Correction", "%",    100,   200,     99,    99,  164,  170, 0, 0 
   ethanolGas        = fuelComposition, "Ethanol Percentage","%",      0,   100,     -1,    -1,   85,  101, 0, 0
   triggers±         = trig_fix,      "Triggers add/sub",     "",   -200,   200,   -100,   -10,   10,  100, 0, 0
   Synch Stat        = synch,          "Synch Status",        "",      0,     5,      0,     0,    5,    5, 0, 0
   tachCount         = tachCount,     "Number Tach Pulses",   "",      0,  1000,     -1,    -1, 1000, 1000, 0, 0   

;-------------------------------------------------------------------------------

[FrontPage]
#if   NARROW_BAND_EGO
   egoLEDs         =  0.0, 1.0,  0.5 ; Voltage settings.
#elif LAMBDA
   egoLEDs         =  1.5, 0.5,  1.0 ; Lambda settings.
#else
   egoLEDs         = 19.7, 9.7, 14.7 ; Afr settings.
#endif

   ; Gauges are numbered left to right, top to bottom.
   ;
   ;    1  2  3  4
   ;    5  6  7  8

   gauge1 = tachometer
   gauge2 = throttleGauge
   gauge3 = pulseWidth1Gauge
#if   NARROW_BAND_EGO
   gauge4 = egoGauge
#elif LAMBDA
   gauge4 = lambda1Gauge
#else
   gauge4 = afr1Gauge
#endif
   gauge5 = mapGauge
#if IAC_GAUGE
   gauge6 = IACgauge
#elif PWM_GAUGE
   gauge6 = PWMIdlegauge
#else
   gauge6 = matGauge
#endif
   gauge7 = advdegGauge
   gauge8 = dwellGauge


   ;----------------------------------------------------------------------------
   ; Indicators
   ;               expr         off-label          on-label, off-bg, off-fg, on-bg, on-fg
   ;   indicator = { tpsaen }, "Not Accelerating", "AE",     cyan,   white,  red,   black
   ;
   ; Look in the new colorScheme.ini for the basic ones, add more or tell me what to add.

   indicator = { ECUType == 1 || ECUType == 2 || ECUType == 3 }, "SET ECU!!",    "ECU Set",  red, black, white, green
   indicator = { crank              }, "Not Cranking", "Cranking",    white, black, black, white
   indicator = { startw             }, "ASE off",      "ASE ON",         white, black, cyan,   black
   indicator = { warmup             }, "WUE off",      "WUE ON",         white, black, blue, white
   indicator = { tpsaen             }, "Accel Enrich",   "Accel Enrich",   white, black, green, black
   indicator = { tpsden             }, "Decel Cut",      "Decel Cut", white, black, green, black
   indicator = { tps > floodClear && crank }, "Flood clear off", "FLOOD CLEAR ON", white, black, red, black
   indicator = { batteryVoltage < 10.5 }, "Battery OK",  "Battery LOW", green, black, red,   black
   indicator = { port0              },  "Port 0 Off",  "Port 0 On",   white, black, red,   black
   indicator = { ignmode            },  "Wasted Spark", "Sequential", white, black, green,   black

;-------------------------------------------------------------------------------

[RunTime]
   barHysteresis = 2.5 ; Seconds
#if CELSIUS
  #if EXPANDED_CLT_TEMP
   coolantBar    = -40,  300
   matBar        = -40,  100
  #else
   coolantBar    = -40,  100
   matBar        = -40,  100
  #endif
#else
  #if EXPANDED_CLT_TEMP
   coolantBar    = -40,  600
   matBar        = -40,  215
  #else
   coolantBar    = -40,  215
   matBar        = -40,  215
  #endif
#endif

   batteryBar    =   6,   15
   dutyCycleBar  =   0,  100
#if   NARROW_BAND_EGO
   egoBar        = 0.0 ,  1.0
#elif LAMBDA
   egoBar        = 0.5,   1.5
#else
   egoBar        = 9.7,  19.7
#endif
   gammaEBar     =   0,  200
   mapBar        =   0,  255
   pulseWidthBar =   0, 25.5
   rpmBar        =   0, 8000
   throttleBar   =   0,  100

   egoCorrBar    =   0,  200
   baroCorrBar   =   0,  200
   warmupCorrBar =   0,  200
   airdenCorrBar =   0,  200
   veCorrBar     =   0,  200
   accCorrBar    =   0,  100

;-------------------------------------------------------------------------------

[Tuning]
#if   NARROW_BAND_EGO
   egoLEDs         =  0.0, 1.0,  0.5 ; Voltage settings.
#elif LAMBDA
   egoLEDs         =  1.5, 0.5,  1.0 ; Lambda settings.
#else
   egoLEDs         = 19.7, 9.7, 14.7 ; Afr settings.
#endif

;  font            = "Lucida Console", 12
;  font            = "Courier", 14
   spotDepth       =   2 ; 0 = no indicators, 1 = Z only, 2 = XYZ indicators.
   cursorDepth     =   2 ; Same as spot depth.

   ; The four radio buttons on the tuning screen select a "page" of six
   ; gauges.  The gauge numbering is the same as the front page, across
   ; then down.
   ;             1  2
   ;             3  4
   ;             5  6
   ;
   ; gaugeColumns allows you to hide or show gauges in column 2 (i.e.,
   ; gauges 2, 4 and 6).

   gaugeColumns = 2 ; Only 1 or 2 are valid.

   ;              Page 1            Page 2             Page 3            Page 4
   pageButtons  = "&EGO",           "&WUE",            "PW&1",           "PW&2"
   gauge1       = tachometer,       tachometer,        tachometer,       tachometer
   gauge2       = mapGauge,         mapGauge,          mapGauge,         mapGauge
#if   NARROW_BAND_EGO
   gauge3       = egoGauge,         egoGauge,          egoGauge,         egoGauge
#elif LAMBDA
   gauge3       = lambda1Gauge,     lambda1Gauge,      lambda1Gauge,     lambda1Gauge
#else
   gauge3       = afr1Gauge,        afr1Gauge,         afr1Gauge,        afr1Gauge
#endif
   gauge4       = egoCorrGauge,     warmupEnrichGauge, pulseWidth1Gauge, pulseWidth2Gauge
   gauge5       = veBucketGauge,    veBucketGauge,     veBucketGauge,    veBucketGauge
   gauge6       = accelEnrichGauge, accelEnrichGauge,  dutyCycle1Gauge,  dutyCycle2Gauge

;-------------------------------------------------------------------------------

[AccelerationWizard]
   tpsDotBar = 0, 100
   mapDotBar = 0, 200

;-------------------------------------------------------------------------------

[BurstMode]
   getCommand       = "a\x00\x06"

[OutputChannels]
   deadValue        = { 0 } ; Convenient unchanging value.

   ochBlockSize     = 130
   ochGetCommand    = "a\x00\x06" ; Lower case so we don't get confused.

   seconds          = scalar, U16,    0, "s",     1.000, 0.0
   secl = { seconds % 256 }, "s" ; For runtime screen.
   pulseWidth1      = scalar, U16,    2, "s",     0.001, 0.0
   pulseWidth2      = scalar, U16,    4, "s",     0.001, 0.0
   pulseWidth       = { pulseWidth1 }, "s" ; For runtime screen.

   rpm              = scalar, U16,    6, "RPM",   1.000, 0.0
   advance          = scalar, S16,    8, "deg",   0.100, 0.0

   ; unsigned char squirt,engine,afrtgt1,afrtgt2;    // afrtgt in afr x 10
   squirt           = scalar, U08,   10, "bit", 1.000, 0.0
   ; Squirt Event Scheduling Variables - bit fields for "squirt" variable above
   ; inj1:    equ    3       ; 0 = no squirt         1 = squirt
   ; inj2:    equ    5       ; 0 = no squirt         1 = squirt
   ; sched1:  equ    2       ; 0 = nothing scheduled 1 = scheduled to squirt
   ; firing1: equ    0       ; 0 = not squirting     1 = squirting
   ; sched2:  equ    4
   ; firing2: equ    1
   firing1          = bits,   U08,   10, [0:0]
   firing2          = bits,   U08,   10, [1:1]
   sched1           = bits,   U08,   10, [2:2]
   inj1             = bits,   U08,   10, [3:3]
   sched2           = bits,   U08,   10, [4:4]
   inj2             = bits,   U08,   10, [5:5]

   engine           = scalar, U08,   11, "bit",   1.000, 0.0
   ; Engine Operating/Status variables - bit fields for "engine" variable above
   ; ready:   equ    0       ; 0 = engine not ready 1 = ready to run
   ; crank:   equ    1       ; 0 = engine not cranking 1 = engine cranking
   ; startw:  equ    2       ; 0 = not in startup warmup 1 = in warmup enrichment
   ; warmup:  equ    3       ; 0 = not in warmup 1 = in warmup
   ; tpsaen:  equ    4       ; 0 = not in TPS acceleration mode 1 = TPS acceleration mode
   ; tpsden:  equ    5       ; 0 = not in deacceleration mode 1 = in deacceleration mode
   ; ignmode: equ    6       ; 0 = wasted spark mode 1= sequential mode (sequencer only)
   ready            = bits,   U08,   11, [0:0]
   crank            = bits,   U08,   11, [1:1]
   startw           = bits,   U08,   11, [2:2]
   warmup           = bits,   U08,   11, [3:3]
   tpsaen           = bits,   U08,   11, [4:4]
   tpsden           = bits,   U08,   11, [5:5]
   ignmode          = bits,   U08,   11, [6:6]
   #if   NARROW_BAND_EGO
     afrtgt1        = scalar, U08,   12, "V",     0.010, 0.0
     afrtgt2        = scalar, U08,   13, "V",     0.010, 0.0
   #elif LAMBDA
     afrtgt1        = scalar, U08,   12, "Lambda",   0.010, 0.0
     afrtgt2        = scalar, U08,   13, "Lambda",   0.010, 0.0
   #else
     afrtgt1        = scalar, U08,   12, "AFR",   0.100, 0.0
     afrtgt2        = scalar, U08,   13, "AFR",   0.100, 0.0
   #endif

   ; unsigned char wbo2_en1,wbo2_en2; // from wbo2 - indicates whether wb afr valid
   wbo2_en1         = scalar, U08,   14, "",      1.000, 0.0
   wbo2_en2         = scalar, U08,   15, "",      1.000, 0.0

   ; int baro,map,mat,clt,tps,batt,ego1,ego2,knock, // baro   - kpa x 100
   ;                                                // map    - kpa x 10
   ;                                                // mat, clt deg(C/F)x 10
   ;                                                // tps    - % x 10
   ;                                                // batt   - vlts x 10
   ;                                                // ego1,2 - afr x 10
   ;                                                // knock  - volts x 100
   barometer        = scalar, S16,   16, "kPa",   0.100, 0.0
   map              = scalar, S16,   18, "kPa",   0.100, 0.0
#if CELSIUS
   mat              = scalar, S16,   20, "°C",   0.05555, -320.0
   coolant          = scalar, S16,   22, "°C",   0.05555, -320.0
#else
   mat              = scalar, S16,   20, "°F",    0.100, 0.0
   coolant          = scalar, S16,   22, "°F",    0.100, 0.0
#endif
   tps              = scalar, S16,   24, "%",     0.100, 0.0
   tpsADC           = { tps*10.23 }, "ADC" ; Fake for calibrator and file indexing.
   throttle         = { tps }, "%"
   batteryVoltage   = scalar, S16,   26, "v",     0.100, 0.0
   afr1             = scalar, S16,   28, "AFR",   0.100, 0.0
   afr2             = scalar, S16,   30, "AFR",   0.100, 0.0
   lambda1          = { afr1 / 14.7 }, "Lambda"
   lambda2          = { afr2 / 14.7 }, "Lambda"
   knock            = scalar, S16,   32, "v",     0.010, 0.0

   ; egocor1,egocor2,aircor,warmcor,     // all in %
   egoCorrection1   = scalar, S16,   34, "%",     1.000, 0.0
   egoCorrection    = { ( egoCorrection1 + egoCorrection2) / 2 }, "%" ; Alias for old gauges.
   egoCorrection2   = scalar, S16,   36, "%",     1.000, 0.0
   airCorrection    = scalar, S16,   38, "%",     1.000, 0.0
   warmupEnrich     = scalar, S16,   40, "%",     1.000, 0.0

   fuelComposition  = { (fuelCorrection - 100)*1.587 }, % ; works with default sensor values

   ; tpsaccel,tpsfuelcut,barocor,gammae, // tpsaccel - acc enrich(.1 ms units)
   ;                                     // tpsfuelcut - %
   ;                                     // barcor,gammae - %
   accelEnrich      = scalar, S16,   42, "msec",    0.100, 0.0
   tpsfuelcut       = scalar, S16,   44, "%",     1.000, 0.0
   baroCorrection   = scalar, S16,   46, "%",     1.000, 0.0
   gammaEnrich      = scalar, S16,   48, "%",     1.000, 0.0

   ;  vecurr1,vecurr2,iacstep,cold_adv_deg;           // vecurr - %
   ;                                                  // iacstep - steps
   ;                                                  // cold_adv_deg - deg x 10
   veCurr1          = scalar, S16,   50, "%",     1.000, 0.0
   veCurr2          = scalar, S16,   52, "%",     1.000, 0.0
   veCurr           = { veCurr1 }, "%" ; For runtime display.
   iacstep          = scalar, S16,   54, "",      1.000, 0.0
   idleDC           = { iacstep } ; Close enough.
   coldAdvDeg       = scalar, S16,   56, "deg",   0.100, 0.0
   tpsDOT           = scalar, S16,   58, "%/sec",   1.000, 0.0
   mapDOT           = scalar, S16,   60, "kPa/sec", 1.000, 0.0
   dwell            = scalar, S16,   62, "msec",    0.100, 0.0
   maf              = scalar, U16,   64, "g/sec",   0.010, 0.0
   kpa              = scalar, S16,   66, "kPa",   0.100, 0.0 ; Blend of MAP, MAFMAP and TPS, depends on algorithm
   mafDOT           = scalar, S16,   68, "g/sec2",  0.100, 0.0
   fuelCorrection   = scalar, S16,   70, "%",     1.000, 0.0 ; Percent alcohol in fuel.

   portStatus       = scalar, U08,   72, "bit",   1.000, 0.0 ; Spare port status bits
   port0            = bits,   U08,   72, [0:0]
   port1            = bits,   U08,   72, [1:1]
   port2            = bits,   U08,   72, [2:2]
   port3            = bits,   U08,   72, [3:3]
   port4            = bits,   U08,   72, [4:4]
   port5            = bits,   U08,   72, [5:5]
   port6            = bits,   U08,   72, [6:6]

   knockRetard      = scalar, U08,   73, "deg",   0.100, 0.0
   xTauFuelCorr1    = scalar, S16,   74, "%",     1.000, 0.0
   egoV1            = scalar, S16,   76, "Volts", 0.010, 0.0
   egoV2            = scalar, S16,   78, "Volts", 0.010, 0.0
   amcUpdates       = scalar, S16,   80,  "",     1.000, 0.0
   kpaix            = scalar, S16,   82, "kPa",   0.100, 0.0
   xTauFuelCorr2    = scalar, S16,   84, "%",     1.000, 0.0
   vemafmap         = scalar, S16,   86, "%",     0.100, 0.0
   vergm            = scalar, S16,   88, "%",     1.000, 0.0
   mafraw           = scalar, U16,   90, "g/sec", 0.010, 0.0
   mafsensor        = scalar, U16,   92, "g/sec", 0.010, 0.0
   mapmaf           = scalar, U16,   94, "g/sec", 0.010, 0.0
   mafmap           = scalar, S16,   96, "kPa",   0.100, 0.0
   synch            = scalar, U08,   98,  "",     1.000, 0.0 
   spare1           = scalar, S16,  100,  "deg",  0.100, 0.0
   spare2           = scalar, S16,  102,  "",     1.000, 0.0
   trig_fix         = scalar, S16,  104,  "",     1.000, 0.0  
   spare4           = scalar, S16,  106,  "",     1.000, 0.0
   spare5           = scalar, S16,  108,  "",     1.000, 0.0
   spare6           = scalar, S16,  110,  "",     1.000, 0.0
   spare7           = scalar, S16,  112,  "",     1.000, 0.0
   spare8           = scalar, S16,  114,  "",     1.000, 0.0
   spare9           = scalar, S16,  116,  "",     1.000, 0.0
   uspare1          = scalar, U16,  118,  "",     1.000, 0.0
   uspare2          = scalar, U16,  120,  "",     1.000, 0.0
   tachCount        = scalar, U16,  122,  "",     1.000, 0.0
   ospare           = scalar, U08,  124,  "",     1.000, 0.0
   cksum            = scalar, U08,  125,  "",     1.000, 0.0
   deltaT           = scalar, U32,  126,  "uS",   1.000, 0.0 ; Normalized time between trigger pulses,
                                                             ; "fills in" missing teeth.


   accDecEnrich     = { ((accEnrichMS + decEnrichMS)/pulseWidth1*100) + 100 }, "%"
   accDecEnrichPcnt = { accelEnrich/pulseWidth1 + (tpsden ? tpsfuelcut : accelEnrich/pulseWidth1*100)      }, "%"
   accEnrichPcnt    = { 100 + (accelEnrich/pulseWidth1*100)  }, "%"
   accEnrichMS      = { accelEnrich                  }, "msec"
   decEnrichPcnt    = { (tpsden ? tpsfuelcut : 100)  }, "%"
   decEnrichMS      = { (tpsfuelcut/100*pulseWidth1)-pulseWidth1   }, "msec"
    
   time             = { timeNow                                        }, "s"
   rpm100           = { rpm / 100.0                                    }

   altDiv1          = { alternate ? 2 : 1                              }
   altDiv2          = { alternate ? 2 : 1                              }

   cycleTime1       = { (60000.0 / rpm) * (2.0-twoStroke)                }, "ms"
   cycleTime2       = { (60000.0 / rpm) * (2.0-twoStroke)                }, "ms"

#if MS2_SEQ
   dutyCycle1       = { (100.0 * pulseWidth1) / (cycleTime1 / (2.0-ignmode)) }, "%"
   dutyCycle2       = { (100.0 * pulseWidth2) / (cycleTime2 / (2.0-ignmode)) }, "%"
#else 
   nSquirts1        = { nCylinders/divider                             }
   nSquirts2        = { nCylinders/divider                             }
   dutyCycle1       = { 100.0*nSquirts1/altDiv1*pulseWidth1/cycleTime1 }, "%"
   dutyCycle2       = { 100.0*nSquirts2/altDiv2*pulseWidth2/cycleTime2 }, "%"
#endif

#if   NARROW_BAND_EGO
   egoVoltage = { egoV1            }, "V"      ; For LED bars...
   egoVoltage2 = { egoV2            }, "V"      ; For LED bars...
#elif LAMBDA
   egoVoltage = { lambda1          }, "Lambda" ; For LED bars...
#else
   egoVoltage = { afr1             }, "AFR"    ; For LED bars...
   egoVoltage2 = { afr2             }, "AFR"    ; For LED bars...
#endif
;     pageSize =  130

;-------------------------------------------------------------------------------
;--  The entries are saved in the datalog file in the order in which they     --
;--  appear in the list below.                                                --
;--                                                                           --
;--   Channel - Case sensitive name of output channel to be logged.           --
;--   Label   - String written to header line of log.  Be careful             --
;--             about changing these, as programs like MSLVV and              --
;--             MSTweak key off specific column names.                        --
;--   Type    - Data type of output, converted before writing.                --
;--   Format  - C-style output format of data.                                --

[Datalog]
   ;       Channel          Label          Type    Format
   ;       --------------   ----------     -----   ------
   entry = time,            "Time",        float,  "%.3f"
   entry = seconds,         "SecL",        int,    "%d"
   entry = rpm,             "RPM",         int,    "%d"
   entry = map,             "MAP",         float,  "%.1f"
   entry = kpaix,           "Tbl Indx",    float,  "%.1f"
   entry = maf,             "MAF",         float,  "%.2f"
   entry = throttle,        "TP",          float,  "%.1f"
   entry = batteryVoltage,  "vBatt",       float,  "%.2f"

#if   NARROW_BAND_EGO
   entry = egoVoltage,      "O2",          float,  "%.3f"
#elif LAMBDA
   entry = lambda1,         "Lambda",      float,  "%.3f"
#else
   entry = afr1,            "AFR",         float,  "%.2f"
#endif
   entry = mat,             "IAT",         float,  "%.1f"
   entry = coolant,         "CLT",         float,  "%.1f"
   entry = engine,          "Engine",      int,    "%d"

   entry = egoCorrection,   "Gego",        int,    "%d"
   entry = airCorrection,   "Gair",        int,    "%d"
   entry = warmupEnrich,    "Gwarm",       int,    "%d"
   entry = baroCorrection,  "Gbaro",       int,    "%d"
   entry = gammaEnrich,     "Gammae",      int,    "%d"
   entry = accDecEnrich,    "AccelEnrich", int,    "%d"

   entry = veCurr1,         "Gve",         int,    "%d"
   entry = pulseWidth1,     "PW",          float,  "%.3f"
   entry = dutyCycle1,      "DutyCycle1",  float,  "%.1f"

   entry = veCurr2,         "Gve2",        int,    "%d"
   entry = pulseWidth2,     "PW2",         float,  "%.3f"
   entry = dutyCycle2,      "DutyCycle2",  float,  "%.1f"

   entry = advance,         "SparkAdv",    float,  "%.1f"
   entry = knockRetard,     "knockRet",    float,  "%.1f"
   entry = coldAdvDeg,      "ColdAdv",     float,  "%.1f"
   entry = dwell,           "Dwell",       float,  "%.2f"
   entry = tpsDOT,          "tpsDOT",      int,    "%d"
   entry = mapDOT,          "mapDOT",      int,    "%d"
   entry = iacstep,         "IAC",         int,    "%d"
   entry = deltaT,          "deltaT",      float,  "%.0f"
   entry = trig_fix,        "Trigger±",    int,    "%d"
   entry = synch,           "Sync Stat",   int,    "%d"
   entry = tachCount,       "tachCount",   int,    "%d"
   entry = xTauFuelCorr1,   "XTau1",       int,    "%d"
   entry = xTauFuelCorr2,   "XTau2",       int,    "%d"
   entry = mafmap,          "map_frm_maf", float,  "%.1f"
   entry = mapmaf,          "maf_frm_map", float,  "%.1f"
   entry = vemafmap,        "VEmfmp",      float,  "%.1f"
   entry = vergm,           "VErgm",       int,    "%d"
   entry = afrtgt1,         "AFRtrgt1",    float,  "%.2f"
   entry = knock,           "knck-V",      float,  "%.2f"

   
;-------------------------------------------------------------------------------
#if MS2_SEQ
[PortEditor]
    ; map the arrays and supply the labels.
    ; all arrays are expected to be the same length in the first dimension
    ; thus a [ 7] array will be 7 ports in length and expect 7 labels
    ; The second dimension will drive the number of conditions per array.
    ; thus a [7x2] array will have 2 conditions joined by the conditionRelationship.
    ; a [7x3] will have up to 3 conditions.
    portEditor = std_port_edit, "Output Port Settings"
    ;   topicHelp = "http://www.megamanual.com/mt28.htm#sp"
        ; 1st the array constant, then the labels in the index order.
        enabledPorts = psEnabled, "Green Pin 7(IDL)", "Red Pin 31", "Green Pin 16", "Green Pin 17", "Jumpr IAC1 to IAC2A/B", "Jumpr IAC2 to IAC1A/B", "Red Pin 20"
        outputOffset = psOutOffset
        outputSize   = psOutSize
        operators    = psCondition, "<", "=", ">" ; the actual ASCII value of the operator will be sent to the controller
        hysteresis = psHysteresis
        threshold = psThreshold
        powerOnValue = psInitValue
        triggerValue = psPortValue
        conditionRelationship = psConnector, " ", "|", "&"
#endif