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speeduino-personal
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Working degrees F in TunerStudio

This commit is contained in:
Josh Stewart 2016-03-29 21:02:02 +11:00
parent 38f1ebc063
commit a06939f4be
1 changed files with 37 additions and 14 deletions
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51
reference/speeduino.ini
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@ -211,7 +211,7 @@ page = 4
#if CELSIUS #if CELSIUS
IdleAdvCLT = scalar, U08, 9, "C", 1, -40, -40, 102, 1 IdleAdvCLT = scalar, U08, 9, "C", 1, -40, -40, 102, 1
#else #else
IdleAdvCLT = scalar, U08, 9, "F", 0.555, -8, -40, 215, 0 IdleAdvCLT = scalar, U08, 9, "F", 1.8, -22.23, -40, 215, 0
#endif #endif
IdleDelayTime = scalar, U08, 10, "sec", 1, 0, 0, 5, 0 IdleDelayTime = scalar, U08, 10, "sec", 1, 0, 0, 5, 0
StgCycles = scalar, U08, 11, "cycles", 1, 0, 0, 255, 0 StgCycles = scalar, U08, 11, "cycles", 1, 0, 0, 255, 0
@ -241,7 +241,11 @@ page = 4
;TPS based acceleration enrichment ;TPS based acceleration enrichment
taeBins = array, U08, 23, [ 4], "%/s", 10.0, 0.0, 0.00, 2550.0, 0 taeBins = array, U08, 23, [ 4], "%/s", 10.0, 0.0, 0.00, 2550.0, 0
taeRates = array, U08, 27, [ 4], "%", 1.0, 0.0, 0.00, 255.0, 0 ; 4 bytes taeRates = array, U08, 27, [ 4], "%", 1.0, 0.0, 0.00, 255.0, 0 ; 4 bytes
#if CELSIUS
wueRates = array, U08, 31, [10], "C", 1.0, 0.0, 100.0, 255.0, 0 wueRates = array, U08, 31, [10], "C", 1.0, 0.0, 100.0, 255.0, 0
#else
wueRates = array, U08, 31, [10], "F", 1.8, 17.77, 100.0, 255.0, 0 ; No -40 degree offset here
#endif
;Dwell config options ;Dwell config options
dwellLim = scalar, U08, 41, "ms", 1, 0, 0, 32, 0 dwellLim = scalar, U08, 41, "ms", 1, 0, 0, 32, 0
dwellRates = array, U08, 42, [6], "%", 1.0, 0.0, 0.00, 255.0, 0 dwellRates = array, U08, 42, [6], "%", 1.0, 0.0, 0.00, 255.0, 0
@ -250,7 +254,7 @@ page = 4
#if CELSIUS #if CELSIUS
iatRetBins = array, U08, 48, [ 6], "C", 1.0, 0.0, 0.00, 255.0, 0 iatRetBins = array, U08, 48, [ 6], "C", 1.0, 0.0, 0.00, 255.0, 0
#else #else
iatRetBins = array, U08, 48, [ 6], "F", 1.0, 0.0, 0.00, 255.0, 0 iatRetBins = array, U08, 48, [ 6], "F", 1.8, 17.77, 0.00, 255.0, 0 ; No -40 degree offset here
#endif #endif
iatRetRates = array, U08, 54, [ 6], "deg", 1.0, 0.0, 0.00, 255.0, 0 iatRetRates = array, U08, 54, [ 6], "deg", 1.0, 0.0, 0.00, 255.0, 0
;Decelleration Fuel Cut Off (DFCO) ;Decelleration Fuel Cut Off (DFCO)
@ -290,9 +294,9 @@ page = 6
egoKI = scalar, U08, 2, "%", 1.0, 0.0, 0.0, 200.0, 0 ; * ( 1 byte) egoKI = scalar, U08, 2, "%", 1.0, 0.0, 0.0, 200.0, 0 ; * ( 1 byte)
egoKD = scalar, U08, 3, "%", 1.0, 0.0, 0.0, 200.0, 0 ; * ( 1 byte) egoKD = scalar, U08, 3, "%", 1.0, 0.0, 0.0, 200.0, 0 ; * ( 1 byte)
#if CELSIUS #if CELSIUS
egoTemp = scalar, U08, 4, "°C", 0.555, -72, -40, 102.0, 0 egoTemp = scalar, U08, 4, "°C", 1.0, -40, -40, 102.0, 0
#else #else
egoTemp = scalar, U08, 4, "°F", 1.0, -40, -40, 215.0, 0 egoTemp = scalar, U08, 4, "°F", 1.8, -22.23, -40, 215.0, 0
#endif #endif
egoCount = scalar, U08, 5, "", 4.0, 0.0, 4.0, 255.0, 0 ; * ( 1 byte) egoCount = scalar, U08, 5, "", 4.0, 0.0, 4.0, 255.0, 0 ; * ( 1 byte)
egoDelta = scalar, U08, 6, "%", 1.0, 0.0, 0.0, 255.0, 0 ; * ( 1 byte) egoDelta = scalar, U08, 6, "%", 1.0, 0.0, 0.0, 255.0, 0 ; * ( 1 byte)
@ -306,7 +310,11 @@ page = 6
egoLoadMin = scalar, U08, 14, "%", 1, 0, 0, 120, 0 egoLoadMin = scalar, U08, 14, "%", 1, 0, 0, 120, 0
brvBins = array, U08, 15, [6], "V", 0.1, 0, 6, 24, 1 ; Bins for the battery reference voltage brvBins = array, U08, 15, [6], "V", 0.1, 0, 6, 24, 1 ; Bins for the battery reference voltage
injBatRates = array, U08, 21, [6], "%", 1, 0, 0, 255, 0 ;Values for injector pulsewidth vs voltage injBatRates = array, U08, 21, [6], "%", 1, 0, 0, 255, 0 ;Values for injector pulsewidth vs voltage
#if CELSIUS
airDenBins = array, U08, 27, [9], "C", 1.0, -40, -40, 215, 0 ; Bins for the air density correction curve airDenBins = array, U08, 27, [9], "C", 1.0, -40, -40, 215, 0 ; Bins for the air density correction curve
#else
airDenBins = array, U08, 27, [9], "F", 1.8, -22.23, -40, 215, 0 ; Bins for the air density correction curve
#endif
airDenRates = array, U08, 36, [9], "%", 1.0, 0.0, 0, 255, 0 ; Values for the air density correction curve airDenRates = array, U08, 36, [9], "%", 1.0, 0.0, 0, 255, 0 ; Values for the air density correction curve
; PWM Frequencies ; PWM Frequencies
@ -343,10 +351,18 @@ page = 7
iacCLValues = array, U08, 0, [10], "RPM", 1.0, 0.0, 100.0, 255, 0 iacCLValues = array, U08, 0, [10], "RPM", 1.0, 0.0, 100.0, 255, 0
iacOLStepVal = array, U08, 10, [10], "Steps", 3, 0, 0, 765, 0 iacOLStepVal = array, U08, 10, [10], "Steps", 3, 0, 0, 765, 0
iacOLPWMVal = array, U08, 20, [10], "Duty %", 1.0, 0, 0, 100, 0 iacOLPWMVal = array, U08, 20, [10], "Duty %", 1.0, 0, 0, 100, 0
#if CELSIUS
iacBins = array, U08, 30, [10], "C", 1.0, -40, -40, 215, 0 iacBins = array, U08, 30, [10], "C", 1.0, -40, -40, 215, 0
#else
iacBins = array, U08, 30, [10], "F", 1.8, -22.23, -40, 215, 0
#endif
iacCrankSteps= array, U08, 40, [4], "Steps", 3, 0, 0, 765, 0 iacCrankSteps= array, U08, 40, [4], "Steps", 3, 0, 0, 765, 0
iacCrankDuty = array, U08, 44, [4], "Duty %", 1.0, 0, 0, 100, 0 iacCrankDuty = array, U08, 44, [4], "Duty %", 1.0, 0, 0, 100, 0
#if CELSIUS
iacCrankBins = array, U08, 48, [4], "C", 1.0, -40, -40, 215, 0 iacCrankBins = array, U08, 48, [4], "C", 1.0, -40, -40, 215, 0
#else
iacCrankBins = array, U08, 48, [4], "F", 1.8, -22.23, -40, 215, 0
#endif
iacAlgorithm = bits , U08, 52, [0:2], "None", "On/Off", "PWM", "INVALID", "Stepper", "INVALID", "INVALID", "INVALID" iacAlgorithm = bits , U08, 52, [0:2], "None", "On/Off", "PWM", "INVALID", "Stepper", "INVALID", "INVALID", "INVALID"
iacStepTime = bits , U08, 52, [3:5], "1", "2", "3", "4", "5", "6" iacStepTime = bits , U08, 52, [3:5], "1", "2", "3", "4", "5", "6"
@ -356,7 +372,7 @@ page = 7
#if CELSIUS #if CELSIUS
iacFastTemp = scalar, U08, 53, "C", 1.0, -40, -40, 215, 0 iacFastTemp = scalar, U08, 53, "C", 1.0, -40, -40, 215, 0
#else #else
iacFastTemp = scalar, U08, 53, "F", 1.8, -4.44, -40, 215, 0 iacFastTemp = scalar, U08, 53, "F", 1.8, -22.23, -40, 215, 0
#endif #endif
iacStepHome = scalar, U08, 54, "Steps", 3, 0, 0, 765, 0 iacStepHome = scalar, U08, 54, "Steps", 3, 0, 0, 765, 0
@ -375,8 +391,8 @@ page = 7
fanSP = scalar, U08, 57, "°C", 1.0, -40, -40, 215.0, 0 fanSP = scalar, U08, 57, "°C", 1.0, -40, -40, 215.0, 0
fanHyster = scalar, U08, 58, "°C", 1.0, -40, -40, 215.0, 0 fanHyster = scalar, U08, 58, "°C", 1.0, -40, -40, 215.0, 0
#else #else
fanSP = scalar, U08, 57, "°F", 1.0, -40, -40, 215.0, 0 fanSP = scalar, U08, 57, "°F", 1.8, -22.23, -40, 215.0, 0
fanHyster = scalar, U08, 58, "°F", 1.0, -40, -40, 215.0, 0 fanHyster = scalar, U08, 58, "°F", 1.8, -22.23, -40, 215.0, 0
#endif #endif
unused7-59 = scalar, U08, 59, "RPM", 100.0, 0.0, 100, 25500, 0 unused7-59 = scalar, U08, 59, "RPM", 100.0, 0.0, 100, 25500, 0
unused7-60 = scalar, U08, 60, "RPM", 100.0, 0.0, 100, 25500, 0 unused7-60 = scalar, U08, 60, "RPM", 100.0, 0.0, 100, 25500, 0
@ -838,7 +854,11 @@ page = 8
; Standard duty table for PWM valves ; Standard duty table for PWM valves
curve = iacPwm_curve, "IAC PWM Duty" curve = iacPwm_curve, "IAC PWM Duty"
columnLabel = "Coolant Temperature", "Valve" columnLabel = "Coolant Temperature", "Valve"
#if CELSIUS
xAxis = -40, 215, 6 xAxis = -40, 215, 6
#else
xAxis = -40, 315, 6
#endif
yAxis = 0, 100, 4 yAxis = 0, 100, 4
xBins = iacBins, coolant xBins = iacBins, coolant
yBins = iacOLPWMVal yBins = iacOLPWMVal
@ -853,7 +873,11 @@ page = 8
curve = iacStep_curve, "IAC Stepper Motor" curve = iacStep_curve, "IAC Stepper Motor"
columnLabel = "Coolant Temperature", "Motor" columnLabel = "Coolant Temperature", "Motor"
xAxis = -40, 120, 6 #if CELSIUS
xAxis = -40, 215, 6
#else
xAxis = -40, 315, 6
#endif
yAxis = 0, 850, 4 yAxis = 0, 850, 4
xBins = iacBins, coolant xBins = iacBins, coolant
yBins = iacOLStepVal yBins = iacOLStepVal
@ -1140,13 +1164,8 @@ page = 8
mapaccden = bits, U08, 2, [7:7] mapaccden = bits, U08, 2, [7:7]
dwell = scalar, U08, 3, "ms", 0.100, 0.000 dwell = scalar, U08, 3, "ms", 0.100, 0.000
map = scalar, U08, 4, "kpa", 2.000, 0.000 map = scalar, U08, 4, "kpa", 2.000, 0.000
#if CELSIUS
iatRaw = scalar, U08, 5, "°C", 1.000, 0.000 iatRaw = scalar, U08, 5, "°C", 1.000, 0.000
coolantRaw = scalar, U08, 6, "°C", 1.000, 0.000 coolantRaw = scalar, U08, 6, "°C", 1.000, 0.000
#else
iatRaw = scalar, U08, 5, "°F", 1.800, 32.000
coolantRaw = scalar, U08, 6, "°F", 1.800, 32.000
#endif
tpsADC = scalar, U08, 7, "ADC", 1.000, 0.000 tpsADC = scalar, U08, 7, "ADC", 1.000, 0.000
batteryVoltage = scalar, U08, 8, "V", 0.100, 0.000 batteryVoltage = scalar, U08, 8, "V", 0.100, 0.000
afr = scalar, U08, 9, "O2", 0.100, 0.000 afr = scalar, U08, 9, "O2", 0.100, 0.000
@ -1174,9 +1193,13 @@ page = 8
; pre-defined variables, search for "???" and you'll see them. ; pre-defined variables, search for "???" and you'll see them.
accDecEnrich = { accelEnrich + ((engine & 0b00100000) ? tdePct : 100) } accDecEnrich = { accelEnrich + ((engine & 0b00100000) ? tdePct : 100) }
#if CELSIUS
coolant = { coolantRaw - 40 } ; Coolant sensor temperature in user units. coolant = { coolantRaw - 40 } ; Coolant sensor temperature in user units.
iat = { iatRaw - 40 } ; Manifold temperature in user units. iat = { iatRaw - 40 } ; Manifold temperature in user units.
; egoVoltage = { egoADC / 255.0 * 5.0 } ; EGO sensor voltage. #else
coolant = { (coolantRaw - 40) * 1.8 + 32 } ; Coolant sensor temperature in user units.
iat = { (iatRaw - 40) * 1.8 + 32 } ; Manifold temperature in user units.
#endif
time = { timeNow } ; "timeNow" is a parameterless built-in function. time = { timeNow } ; "timeNow" is a parameterless built-in function.
seconds = { secl }; seconds = { secl };