;-------------------------------------------------------------------------------
; #alert "alert text goes here - if uncommented, it will be displayed in a pop-up dialog whever a project using this INI is opened"
; INI date: May30/08 12:52PM PDT
[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 2.88600 " ; 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 to 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
; ------ -------- -----
; - char = S08 U08 1
; - int = S16 U16 2
; - long = S32 U32 4
;
; 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
[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 = 994, 946
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" ; *
ICCrankTrigger = bits , U08, 2, [1:2], "Calculated", "Trigger Return", "Trigger Rise", "INVALID" ; *
ICIgnOption = bits , U08, 2, [4:5], "Standard Coil Charge", "EDIS", "EDIS Multispark", "INVALID" ; *
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", "INVALID" ; * ( 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, 500.00, 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
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
#else
tempTable = array , S16, 470, [ 10], "°F", 0.10000, 0.00000,-40.00, 200.00, 1
#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)
Dtpred_Gain = scalar, S16, 542, "%", 1.00000, 0.00000, -200.0, 200.0, 0 ; * ( 2 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, "", 1.00000, 0.00000, 0.00, 4000.00, 0 ; * ( 1 byte)
#if CELSIUS
IdleHyst = scalar, S16, 554, "°C", 0.05555, -320.000, -40.0, 150.0, 1 ; * ( 2 bytes)
#else
IdleHyst = scalar, S16, 554, "°F", 0.10000, 0.00000, -40.0, 300.0, 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
IACcoldtmp = scalar, S16, 560, "°C", 0.05555, -320.000, -40.0, 150.0, 1 ; * ( 2 bytes)
#else
IACcoldtmp = scalar, S16, 560, "°F", 0.10000, 0.00000,-40.00, 300.00, 1
#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", "Single Wide Band", "Dual Wide Band", "INVALID", "INVALID", "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
egoTarget = 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", "INVALID", ; *
MAFpin = bits , U08, 600, [4:5], "MAF on MAP pin", "MAF on Baro Pin", "MAF on Knock Pin", "INVALID" ; *
DualSpkOptn = bits , U08, 601, [0:3] "No Dual 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)
#if CELSIUS
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)
#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
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)
alternate = bits, U08, 611, [0:0], "Simultaneous", "Alternating" ; * ( 1 byte)
injOpen = scalar, U08, 612, "msec", 0.10000, 0.00000, 0.00, 25.50, 1 ; * ( 1 byte)
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)
battFac = scalar, U08, 616, "ms/v", 0.0166667, 0.00000, 0.00, 1.00, 2 ; * ( 1 byte)
twoStroke = bits, U08, 617, [0:0], "Four-stroke", "Two-stroke" ; *
injType = bits, U08, 618, [0:0], "Port Injection", "Throttle Body" ; *
nInjectors = bits, U08, 619, [0:4], "INVALID" ; *
OddAng = scalar, S16, 620, "degrees", 0.10000, 0.00000,-350.0, 350.00, 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, [0:0], "Single Table", "Dual Table" ; *
algorithm = bits, U08, 630, [0:1], "Speed Density", "Blend SD/Alpha-N", "Pure Alpha-N", "INVALID" ; *
an_direction = bits, U08, 630, [4:5], "Blend SD (hi_rpm)/Alpha-N (lo_rpm)","Blend SD (lo_rpm)/Alpha-N (hi_rpm)". "INVALID", "INVALID";
IgnAlpha = scalar, U08, 631, "", 1.00000, 0.00000, 0.00, 255.00, 0 ; U ( 1 byte) UNUSED
AfrAlpha = scalar, U08, 632, "", 1.00000, 0.00000, 0.00, 255.00, 0 ; U ( 1 byte) UNUSED
AFRStoich = scalar, U08, 633, "AFR", 0.10000, 0.00000, 0.00, 20.00, 1 ; * ( 1 byte)
AFRStoichWB = scalar, U08, 633, "AFR", 0.10000, 0.00000, 0.00, 20.00, 1 ; * ( 1 byte)
AFRStoichNB = 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)
ECUType = scalar, U08, 744, "1=MS-II, 2=MicroSquirt", 1.00000, 0.00000, 0.00, 9.00, 0 ; * ( 1 byte)
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)
mapdotSample = 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"
InjStart = scalar, U08, 752, "%", 1.00000, 0.00000, 0.00, 255.00, 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, [0:0], "Disabled", "Enabled" ; * ( 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 )
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 )
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
fuelSpkDel1 = scalar, S16, 980, "deg", 0.10000, 0.00000,-45.00, 45.00, 1
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)
; pageSize = 994
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
matTemps = array , S16, 658, [ 6], "°C", 0.05555, -320.000,-40.00, 150.00, 1 ; * ( 12 bytes)
#else
matTemps = array , S16, 658, [ 6], "°F", 0.10000, 0.00000,-40.00, 300.00, 1
#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", "Warm-up + Accel/Decel", "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, 5.00, 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, 5.00, 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)
ipada = array, S16, 768, [ 48], "", 1.00000, 0.00000, 0.00, 300, 0 ; * ( 96 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
matCorrTemps = array , S16, 876, [ 6], "°C", 0.05555, -320.000,-40.00, 150.00, 1 ; * ( 12 bytes)
#else
matCorrTemps = array , S16, 876, [ 6], "°F", 0.10000, 0.00000,-40.00, 300.00, 1
#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, [0:0], "Use MAP only", "Adjust MAP for Baro" ; * ( 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)
; pageSize = 946
[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}
subMenu = std_port_edit, "Spare &Port Settings", 0, { ECUType == 1 || ECUType == 2}
subMenu = std_separator, ;----------------------------------------------
subMenu = injChars, "I&njector Characteristics", 0, { ECUType == 1 || ECUType == 2}
subMenu = std_injection, "Injection &Control", 0, { ECUType == 1 || ECUType == 2}
subMenu = revLimiter, "&Rev Limiter", 0, { ECUType == 1 || ECUType == 2}
subMenu = aseSettings, "After&Start Enrichment" , 0, { ECUType == 1 || ECUType == 2}
subMenu = accSettings, "Acce&l Enrichment Config", 0, { ECUType == 1 || ECUType == 2}
subMenu = otherFuel, "&Other Fuel Settings", 0, { ECUType == 1 || ECUType == 2}
subMenu = baroCorrection, "2-Point &Barometric Correction", 0, { ECUType == 1 || ECUType == 2}
subMenu = flexFuelSettings,"&Flex Fuel", 0, { ECUType == 1 || ECUType == 2}
subMenu = egoControl, "&EGO Control", 0, { ECUType == 1 || ECUType == 2}
subMenu = amcSettings, "Automatic &Mixture Control", 0, { ECUType == 1 || ECUType == 2}
subMenu = std_separator ;----------------------------------------------
subMenu = alphaNOptions, "&Alpha-N Blending", 0, { algorithm > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = MAFSettings, "MAP vrs. MAF &Usage", 0, { ECUType == 1 || ECUType == 2}
menuDialog = main
menu = "&Ignition Set-Up"
subMenu = ignitionOptions, "&Base Ignition Settings", 0, { ECUType == 1 || ECUType == 2}
subMenu = dwellSettings, "D&well Settings", 0, { ECUType == 1 || ECUType == 2}
subMenu = AdvncdignitionOptions, "&Advanced Ignition Options",0, { ECUType == 1 || ECUType == 2}
subMenu = knockThreshold, "&Knock Threshold", 0, { ECUType == 1 || ECUType == 2}
menuDialog = knockThreshold
menu = "&Settings"
subMenu = knockSettings, "&Knock Sensor Settings", 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 != 1 && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable1Tbl, "&AFR Table 1 (MAP/Baro)", 0, { egoType >= 3 && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = veTable2Tbl, "V&E Table 2 (MAP/baro)", 0, { MAFOption != 1 && dualTable && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable2Tbl, "AFR &Table 2 (MAP/Baro)", 0, { egoType >= 3 && dualTable && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = ignitionTbl, "&Spark Advance Table (MAP/Baro)",0, { VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
#else
subMenu = veTable1Tbl, "VE Table &1 (MAP)", 0, { MAFOption != 1 && VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable1Tbl, "A&FR Table 1 (MAP)", 0, { egoType >= 3 && VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
subMenu = veTable2Tbl, "VE Table &2 (MAP)", 0, { MAFOption != 1 && dualTable && VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable2Tbl, "AF&R Table 2 (MAP)" 0, { egoType >= 3 && dualTable && VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
subMenu = ignitionTbl, "S&park Advance Table (MAP)", 0, { VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
#endif
menuDialog = main
menu = "Othe&r Tables"
subMenu = tempTableBins, "&Temperature Table Values", 0, { ECUType == 1 || ECUType == 2}
subMenu = alphaMAPTbl, "&Alpha-N MAP Table", 0, { algorithm > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = barometerCorr, "Barometric &Correction", 0, { CWOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = std_separator ;----------------------------------------------
subMenu = primingPW, "Pri&ming Pulse", 0, { CWOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = crankingPW, "Cra&nking Pulse", 0, { CWOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = asePct, "A&SE Percentage", 0, { CWOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = aseTaper, "AS&E Taper", 0, { CWOption > 0 && (ECUType == 1 || ECUType == 2)}
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}
#if MAPbaro
subMenu = std_separator ;----------------------------------------------
subMenu = veTable1Map, "VE &Table 1 (MAP/Baro)", 0, { MAFOption != 1 && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = veTable2Map, "VE T&able 2 (MAP/Baro)", 0, { MAFOption != 1 && dualTable && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable1Map, "A&FR Ta&ble 1 (MAP/Baro)", 0, { egoType >= 3 && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable2Map, "A&FR Tabl&e 2 (MAP/Baro)", 0, { egoType >= 3 && dualTable && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = ignitionMap, "I&gnition Advance Table (MAP/Baro)", 0, { VEIXOptn > 0 && VEIXOptn > 0 && (ECUType == 1 || ECUType == 2)}
#else
subMenu = std_separator ;----------------------------------------------
subMenu = veTable1Map, "VE Table &1 (MAP)", 0, { MAFOption != 1 && VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
subMenu = veTable2Map, "VE Table &2 (MAP)", 0, { MAFOption != 1 && dualTable && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable1Map, "A&FR Table 1 (MAP)", 0, { egoType >= 3 && VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
subMenu = afrTable2Map, "AF&R Table 2 (MAP)", 0, { egoType >= 3 && dualTable && VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
subMenu = ignitionMap, "&Spark Advance Table (MAP)", 0, { VEIXOptn == 0 && (ECUType == 1 || ECUType == 2)}
#endif
subMenu = std_separator ;----------------------------------------------
subMenu = std_warmup, "&Warmup Wizard", 0, { ECUType == 1 || ECUType == 2}
subMenu = std_accel, "Acce&leration Wizard", 0, { ECUType == 1 || ECUType == 2}
menuDialog = main
menu = "X-Ta&u Tuning"
subMenu = XAccTable, "Puddling Factors (&accel)", 0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = XDecTable, "Puddling Factors (&decel)", 0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = TauAccTable, "Time Factors (a&ccel)", 0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = TauDecTable, "Time Factors (d&ecel)", 0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = XCltTable, "&X (Puddling) Temp. Corrections",0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = TCltTable, "&Tau (Time) Temp. Corrections", 0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = std_separator ;----------------------------------------------
subMenu = xTauSettings, "&MAPdot Settings", 0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = XTrpmsdial, "&RPM Values", 0, { xTauOption > 0 && (ECUType == 1 || ECUType == 2)}
menuDialog = main
menu = "Oth&er Tuning"
subMenu = coldAdvance, "&Cold Advance", 0, { ECUType == 1 || ECUType == 2}
subMenu = std_separator ;----------------------------------------------
subMenu = manifoldTempCorr,"I&AT-Based Fuel Correction", 0, { ECUType == 1 || ECUType == 2}
subMenu = matBasedRetard, "IAT-&Based Timing Retard", 0, { ECUType == 1 || ECUType == 2}
subMenu = std_separator ;----------------------------------------------
subMenu = iacSteps, "I&dle Steps", 0, { IdleCtl == 2 || IdleCtl == 3 || IdleCtl == 5 && (ECUType == 1 || ECUType == 2)}
subMenu = ipwBins, "Idle &PWM Dutycycle", 0, { IdleCtl == 4 }
subMenu = std_separator ;----------------------------------------------
subMenu = alphaMAPMap, "Alpha-&N MAP Table", 0, { algorithm > 0 && (ECUType == 1 || ECUType == 2)}
subMenu = std_separator ;----------------------------------------------
subMenu = MAFtable1, "&MAF Correction Table", 0, { MAFOption > 0 && (ECUType == 1 || ECUType == 2)}
menuDialog = main
menu = "Tools"
subMenu = std_ms2gentherm, "Calibrate T&hermistor Tables...",0, { ECUType == 1 || ECUType == 2}
subMenu = std_ms2geno2, "Calibrate &AFR Table...", 0, { ECUType == 1 || ECUType == 2}
subMenu = sensorCal, "&Sensor Calibration...", 0, { ECUType == 1 || ECUType == 2}
subMenu = std_trigwiz, "Tri&gger Wizard...", 0, { ECUType == 1 || ECUType == 2}
subMenu = injector_test, "&Injector Test Mode", 0, { ECUType == 1 || ECUType == 2}
menu = "Help"
subMenu = helpGeneral, "&MS-II Info"
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 editting other values."
field = "Engine displacement", CID, { ECUType == 1 || ECUType == 2}
field = "Injection Timing Delay", InjStart, { ECUType == 1 || ECUType == 2}
; field = "#System"
; field = "Temperature Units", tempUnits, { ECUType == 1 || ECUType == 2}
field = "Dual Table Use", dualTable, { ECUType == 1 || ECUType == 2}
field = "Barometric Correction", baroCorr, { ECUType == 1 || ECUType == 2}
# set X_TAU_VISIBLE
#if X_TAU_VISIBLE
field = "X-Tau Usage", xTauOption, { ECUType == 1 || ECUType == 2}
#endif
field = "Prime, ASE, WUE & Baro Tables", CWOption, { ECUType == 1 || ECUType == 2}
field = "#Input Smoothing Factors"
field = "MAP/MAF Averaging Lag Factor", mapLF, { ECUType == 1 || ECUType == 2}
field = "RPM Averaging Lag Factor", rpmLF, { ECUType == 1 || ECUType == 2}
field = "TPS Averaging Lag Factor", tpsLF, { ECUType == 1 || ECUType == 2}
field = "Lambda Averaging Lag Factor", egoLF, { ECUType == 1 || ECUType == 2}
field = "CLT/IAT/Battery Lag Factor", adcLF, { ECUType == 1 || ECUType == 2}
field = "Knock Averaging Lag Factor", knkLF, { ECUType == 1 || ECUType == 2}
field = "#Sampling Rates"
field = "TPS Sample Rate", tpsdotSample, { ECUType == 1 || ECUType == 2}
field = "MAP Sample Rate", mapdotSample, { ECUType == 1 || ECUType == 2}
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 > 0 }
field = "Fuel Correction (low)", fuelCorr0, { flexFuel > 0 }
field = "Timing Correction (low)", fuelSpkDel0, { flexFuel > 0 }
field = "Frequency (high)", fuelFreq1, { flexFuel > 0 }
field = "Fuel Correction (high)", fuelCorr1, { flexFuel > 0 }
field = "Timing Correction (high)", fuelSpkDel1, { flexFuel > 0 }
dialog = otherFuel, "Other Fuel Settings"
topicHelp = "http://www.megamanual.com/mt28.htm#so"
field = "#Engine Start Up"
field = "Max. Cranking Speed", crankingRPM, { 1 }
field = "#VE Table Adjustments"
field = "(May have to save MSQ and reload to get to stick)"
field = "Use MAP/baro for tables", VEIXOptn, { 1 }
field = " - Must also set/unset MAPbaro in settings.ini -"
field = "AFR Table Fuel Calc Usage", AFRMult, { 1 }
field = "AFR Stioch. Ratio", AFRStoichNB, { AFRMult == 1 }
field = "AFR Stioch. Ratio", AFRStoichWB, { AFRMult == 2 }
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, "AfterStart Enrichment Settings"
topicHelp = "http://www.megamanual.com/mt28.htm#ss"
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
field = "PWM Time Threshold", injPwmT
field = "!Injector PWM Period", injPwmPd ; !
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
#if NARROW_BAND_EGO
field = "NB Voltage Target", egoTarget, { egoType == 1 || egoType == 2}
#elif LAMBDA
field = "NB Lambda Target", AFRTarget, { egoType == 1 || egoType == 2}
#else
field = "NB AFR Target", AFRTarget, { egoType == 1 || egoType == 2}
#endif
field = "Ignition Events per Step", egoCount, { egoType == 1 || egoType == 2 || egoType > 2 && egoAlgorithm == 0}
field = "Controller Step Size", egoDelta, { egoType == 1 || egoType == 2}
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 }
field = "PID Proportional Gain", egoKP, { egoType > 2 }
field = "Transport Delay 1", egoKdelay1, { egoType > 2 && egoAlgorithm > 0 }
field = "Transport Delay 2", egoKdelay2, { egoType > 2 && egoAlgorithm > 0 }
field = "PID Integral", egoKI, { egoType > 2 && egoAlgorithm > 1 }
field = "PID Derivative", egoKD, { egoType > 2 && egoAlgorithm > 1 }
dialog = amcSettings, "Automatic Mixture Control"
topicHelp = "http://www.megamanual.com/mt28.htm#sm"
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#sa"
field = "Alpha-N Usage", an_direction, {algorithm == 1}
field = "Pure AN to Blend Threshold", alpha_lorpm
field = "Blend to SD Threshold", alpha_hirpm
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 ; !
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 }
field = "!Skip Teeth", No_Skip_Teeth, { triggerTeeth > 0 }
field = "!Delay Teeth", Delay_Teeth, { triggerTeeth > 0 }
field = "#Dual Spark Ignition Options"
field = "!Dual Spark Options", DualSpkOptn
field = "Offset (advance) for Output #2", OddAng
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 = 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 = "Threshold", knock0
field = "Peak", 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 = MAFSettings, "MAF vrs. MAP Usage"
topicHelp = "http://www.megamanual.com/mt28.htm#su"
field = "#See Tables for MAF flow setting"
field = "Enable MAF Use", MAFOption
field = "MAF Hardware Configuration", MAFpin, { MAFOption > 0 }
field = "Note: MAF must NOT be on MAP pin for MAF/MAP blend."
field = "#MAP MAF Blend Settings"
field = "MAP Only Above RPM", MAFRPM1, { MAFOption > 1 }
field = "MAF Only Below RPM", MAFRPM2, { MAFOption > 1 }
field = "Invert above MAP/MAF settings", MAFDir, { MAFOption > 1 }
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:
"
text = "\tHit TAB after entering the value. This forces MegaTune to"
text = "recognize the changed value.
"
text = "\tThen 'Burn to ECU'
"
text = "If that doesn't work:
"
text = "\tChange the value (as above) and immediately save the MSQ file ('File/Save').
"
text = "\tThen reload the file you just saved, and burn it when prompted.
"
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
"
text = "
"
text = "For the\tMPX4115 use\t10.6 and \t121.7
"
text = "\tMPX4250\t\t10.0\t260.0
"
text = "\tMPXH6300\t1.1\t315.5
"
text = "\tGM 3-BAR\t1.1\t315.5
"
text = "\tMPXH6400\t3.5\t416.5
"
text = "
"
text = "(GM 3-bar data from Dave Hartnell, http://www.not2fast.com/electronics/component_docs/MAP_12223861.pdf)
"
text = "
"
text = "\tSensor type\tvLo\tpLo\tvHi\tpHi\tvRef
"
text = "\tMPX4115 \t0.204 v\t15 kPa\t4.794 v\t115 kPa\t5.100 v
"
text = "\tMPX4250 \t0.204 v\t20 kPa\t4.896 v\t250 kPa\t5.100 v
"
text = "\tMPXH6300\t0.306 v\t20 kPa\t4.913 v\t304 kPa\t5.100 v
"
text = "\tGM 3-BAR\t0.631 v\t40 kPa\t4.914 v\t304 kPa\t5.100 v
"
text = "\tMPXH6400\t0.200 v\t20 kPa\t4.800 v\t400 kPa\t5.000 v
"
text = "
"
text = "In general, use values derived from these equations:
"
text = "
"
text = "\tm = (pHi-pLo)/(vHi-vLo)
"
text = "\tpv1 = pLo - m * vLo
"
text = "\tpv2 = pv1 + m * vRef
"
text = "
"
text = "References:
"
text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPX4115A.pdf
"
text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPX4250A.pdf
"
text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPXH6300A.pdf
"
text = "\thttp://www.freescale.com/files/sensors/doc/data_sheet/MPXH6400A.pdf
"
text = "
"
text = "Barometer Sensor Calibration
"
text = "
"
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.
"
text = "
"
text = "Barometric Correction Calibration
"
text = "
"
text = "Correction for barometric effects is performed using the linear function below.
"
text = "
"
text = "\tcorrection = correction_0 + (rate * barometer) / 100
"
text = "
"
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.
"
text = "
"
text = "\tcorrection = 147 + (-47*100) / 100 = 100%"
help = helpGeneral, "MS-II General Help"
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. MegaSquirt-II is an intermediate"
text = "step from the original MegaSquirt towards UltraMegaSquirt.
"
text = "
"
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).
"
text = "
"
text = "For current documentation, click the Web Help button below, or for"
text = "support questions visit http://www.msefi.com/."
;-------------------------------------------------------------------------------
[CurveEditor]
curve = coldAdvance, "Cold Ignition Advance Offset"
topicHelp = "http://www.megamanual.com/mt28.htm#ec"
columnLabel = "Coolant", "Offset"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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 = knockThreshold, "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"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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"
xAxis = -40, 200, 9
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, calcMAP, 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, calcMAP, 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, calcMAP, 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, calcMAP, 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
#if MAPbaro
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
#else
table = ignitionTbl, ignitionMap, "Spark Advance Table", 2
topicHelp = "http://www.megamanual.com/mt28.htm#ap"
xBins = srpm_table, rpm, readonly
yBins = smap_table, calcMAP, readonly
zBins = advanceTable
upDownLabel = "ADVANCING", "RETARDING"
gridHeight = 3.0
gridOrient = 250, 0, 340
#endif
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", "%", 50, 150, -1, -1, 999, 999, 0, 0
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
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
kpabaroGauge = kpaix, "Engine MAP/baro", "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
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
mafGauge = maf, "MAF Air flow", "g/sec", 0, 650, 0, 200, 480, 550, 0, 0
barometerGauge = barometer, "Barometer", "kPa", 60, 120, 0, 20, 200, 245, 1, 0
calcMapGauge = calcMAP, "Estimated MAP", "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, 10000, 300, 500, 9000, 9500, 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
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
; 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
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
#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
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
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 ; FIDLE_GAUGE
gauge6 = matGauge
#endif
gauge6 = voltMeter
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 }, "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
;-------------------------------------------------------------------------------
[RunTime]
barHysteresis = 2.5 ; Seconds
#if CELSIUS
coolantBar = -40, 100
matBar = -40, 100
#else
coolantBar = -40, 215
matBar = -40, 215
#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 = 112
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
; mapaen: equ 6 ; 0 = not in MAP acceleration mode 1 = MAP deaceeleration mode; not implemented
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]
mapaen = bits, U08, 11, [6:6]
afrtgt1 = scalar, U08, 12, "AFR", 0.100, 0.0
afrtgt2 = scalar, U08, 13, "AFR", 0.100, 0.0
; 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 10
; // 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 10
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", 0.100, 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, S16, 64, "g/sec", 0.010, 0.0
calcMAP = scalar, S16, 66, "kPa", 0.100, 0.0 ; Blend of MAP and TPS, depends on algorithm
fuelCorrection = scalar, S16, 68, "%", 1.000, 0.0 ; Percent alcohol in fuel.
portStatus = scalar, U08, 70, "bit", 1.000, 0.0 ; Spare port status bits
port0 = bits, U08, 70, [0:0]
port1 = bits, U08, 70, [1:1]
port2 = bits, U08, 70, [2:2]
port3 = bits, U08, 70, [3:3]
port4 = bits, U08, 70, [4:4]
port5 = bits, U08, 70, [5:5]
port6 = bits, U08, 70, [6:6]
knockRetard = scalar, U08, 71, "deg", 0.100, 0.0
xTauFuelCorr1 = scalar, S16, 72, "%", 1.000, 0.0
egoV1 = scalar, S16, 74, "Volts", 0.010, 0.0
egoV2 = scalar, S16, 76, "Volts", 0.010, 0.0
amcUpdates = scalar, S16, 78, "", 1.000, 0.0
kpaix = scalar, S16, 80, "kPa", 0.100, 0.0
xTauFuelCorr2 = scalar, S16, 82, "%", 1.000, 0.0
spare1 = scalar, S16, 84, "", 1.000, 0.0
spare2 = scalar, S16, 86, "", 1.000, 0.0
trig_fix = scalar, S16, 88, "", 1.000, 0.0
spare4 = scalar, S16, 90, "", 1.000, 0.0
spare5 = scalar, S16, 92, "", 1.000, 0.0
spare6 = scalar, S16, 94, "", 1.000, 0.0
spare7 = scalar, S16, 96, "", 1.000, 0.0
spare8 = scalar, S16, 98, "", 1.000, 0.0
spare9 = scalar, S16, 100, "", 1.000, 0.0
spare10 = scalar, S16, 102, "", 1.000, 0.0
tachCount = scalar, U16, 104, "", 1.000, 0.0
ospare = scalar, U08, 106, "", 1.000, 0.0
cksum = scalar, U08, 107, "", 1.000, 0.0
deltaT = scalar, U32, 108, "uS", 1.000, 0.0 ; Normalized time between trigger pulses,
; "fills in" missing teeth.
accDecEnrich = { accelEnrich + (tpsden ? tpsfuelcut : 100) }, "%"
time = { timeNow }, "s"
rpm100 = { rpm / 100.0 }
altDiv1 = { alternate ? 2 : 1 }
altDiv2 = { alternate ? 2 : 1 }
cycleTime1 = { 60000.0 / rpm * (2.0-twoStroke) }, "ms"
nSquirts1 = { nCylinders/divider }
dutyCycle1 = { 100.0*nSquirts1/altDiv1*pulseWidth1/cycleTime1 }, "%"
cycleTime2 = { 60000.0 / rpm * (2.0-twoStroke) }, "ms"
nSquirts2 = { nCylinders/divider }
dutyCycle2 = { 100.0*nSquirts2/altDiv2*pulseWidth2/cycleTime2 }, "%"
#if NARROW_BAND_EGO
egoVoltage = { egoV1 }, "V" ; For LED bars...
#elif LAMBDA
egoVoltage = { lambda1 }, "Lambda" ; For LED bars...
#else
egoVoltage = { afr1 }, "AFR" ; For LED bars...
#endif
; pageSize = 112
;-------------------------------------------------------------------------------
;-- 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, "MAP/baro", float, "%.1f"
entry = maf, "MAF", float, "%d"
entry = throttle, "TP", int, "%d"
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 = tachCount, "tachCount", int, "%d"
entry = xTauFuelCorr1 "XTau1", int, "%d"
entry = xTauFuelCorr2 "XTau2", int, "%d"
entry = fuelCorrection, "E85fuelCorr", int, "%d"
entry = fuelComposition, "Ethanol%", int, "%d"
entry = afrtgt1, "AFRtrgt1", float, "%.2f"
;-------------------------------------------------------------------------------