mirror of https://github.com/rusefi/speeduino.git
Large re-org in preparation for EEPROM and comms paging work
This commit is contained in:
Josh Stewart
parent
842f6a6e9c
commit
8e002150ee
38
comms.ino
38
comms.ino
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@ -112,36 +112,34 @@ void sendPage()
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case vePage:
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//Need to perform a translation of the values[MAP/TPS][RPM] into the MS expected format
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for(byte x=0;x<64;x++) { response[x] = fuelTable.values[7-x/8][x%8]; }
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response[64] = 0;
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response[65] = 0;
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response[66] = 0;
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response[67] = 0;
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response[68] = 0;
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response[78] = 0;
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response[79] = 0;
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for(byte x=64;x<72;x++) { response[x] = fuelTable.axisX[(x-100)] / 100; } //RPM Bins for VE table
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for(byte y=72;y<80;y++) { response[y] = fuelTable.axisY[7-(y-108)]; } //MAP or TPS bins for VE table
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response[80] = 0;
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response[81] = 0;
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response[82] = 0;
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response[83] = 0;
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response[84] = 0;
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response[85] = 0;
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response[86] = 0;
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response[87] = 0;
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response[88] = 0;
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response[89] = 0;
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response[90] = (byte)req_fuel;
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response[91] = 0;
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response[92] = 0;
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response[93] = 0;
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response[94] = 0;
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response[95] = 0;
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response[96] = 0;
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response[97] = 0;
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response[98] = 0;
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response[99] = 0;
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for(byte x=100;x<108;x++) { response[x] = fuelTable.axisX[(x-100)] / 100; }
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for(byte y=108;y<116;y++) { response[y] = fuelTable.axisY[7-(y-108)]; }
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response[100] = 0;
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response[101] = 0;
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response[102] = 0;
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response[103] = 0;
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response[104] = 0;
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response[105] = 0;
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response[106] = (byte)req_fuel;
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response[107] = 0;
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response[108] = 0;
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response[109] = 0;
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response[110] = 0;
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response[111] = 0;
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response[112] = 0;
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response[113] = 0;
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response[114] = 0; //rpmk (16 bits)
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response[116] = ((engineCylinders-1) * 16) + (1 * 8) + ((engineStrokes / 4) * 4) + 2; // (engineCylinders * 16) + (1 * 8) + ((engineStrokes / 4) * 4) + 4
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response[117] = 0;
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response[118] = 0;
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@ -160,7 +158,7 @@ void sendPage()
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for(byte x=0;x<64;x++) { response[x] = ignitionTable.values[7-x/8][x%8]; }
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for(byte x=64;x<72;x++) { response[x] = ignitionTable.axisX[(x-64)] / 100; }
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for(byte y=72;y<80;y++) { response[y] = ignitionTable.axisY[7-(y-72)]; }
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response[80] = 0;
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response[80] = triggerAngle;
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response[81] = 0;
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response[82] = 0;
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response[83] = 0;
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89
globals.h
89
globals.h
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@ -1,8 +1,10 @@
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#include <Arduino.h>
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byte ms_version = 20;
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byte data_structure_version = 1; //This identifies the data structure when reading / writing.
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//The status struct contains the current values for all 'live' variables
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//In current version this is 64 bytes
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struct statuses {
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volatile boolean hasSync;
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unsigned int RPM;
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@ -12,3 +14,90 @@ struct statuses {
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unsigned long PW; //In uS
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};
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//Page 1 of the config - See the ini file for further reference
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//This mostly covers off variables that are required for fuel
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struct config1 {
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/*
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byte engineCylinders; 1 // May support more than 1 cyl later. Always will assume 1 injector per cylinder.
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byte engineInjectorSize; 80 // In cc/min
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byte engineStoich; 14.7 // Stoichiometric ratio of fuel used
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byte engineStrokes; 4 //Can be 2 stroke or 4 stroke, any other value will cause problems
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byte engineDwell; 3000 //The spark dwell time in uS
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*/
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byte crankCold;
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byte crankHot;
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byte asePct;
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byte aseCount;
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byte wueBins[10];
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byte taeBins1;
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byte taeBins2;
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byte taeBins3;
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byte taeBins4;
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byte taeColdA;
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byte tpsThresh;
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byte taeTime;
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byte tdePct;
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byte egoTemp;
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byte egoCount;
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byte egoDelta;
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byte egoLimit;
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byte reqFuel;
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byte divider;
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byte alternate;
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byte injOpen;
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byte injOCfuel;
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byte injPwmP;
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byte injPwmT;
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byte battFac; //Whether to compensate pulsewidth for battery voltage (ms/v)
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int rpmk;
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byte mapType;
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byte twoStroke;
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byte injType;
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byte nCylinders;
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byte cltType;
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byte matType;
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byte nInjectors;
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byte engineType;
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byte egoType;
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byte algorithm; //"Speed Density", "Alpha-N"
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byte baroCorr;
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byte primePulse;
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byte egoRPM;
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byte fastIdleT; //Fast idle temperature
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byte egoSwitch;
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byte taeColdM;
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};
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//Page 2 of the config - See the ini file for further reference
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//This mostly covers off variables that are required for ignition
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struct config2 {
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byte trigerAngle;
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byte FixAng;
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byte Trim;
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byte CrankAng;
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byte IgHold;
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byte Trig_plus;
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byte TrigCrank;
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byte IgInv;
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byte oddfire;
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byte IdleAdv;
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byte IdleAdvTPS;
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byte IdleAdvRPM;
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byte IdleAdvCLT;
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byte IdleDelayTime;
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byte StgCycles;
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byte dwellcont; //Fixed duty dwell control
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byte dwellcrank;
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byte dwellrun;
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byte triggerTeeth; //The full count of teeth on the trigger wheel if there were no gaps
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byte triggerMissingTeeth; //The size of the tooth gap (ie number of missing teeth)
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};
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@ -6,15 +6,7 @@
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/*
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Need to calculate the req_fuel figure here, preferably in pre-processor macro
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*/
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#define engineCapacity 148 // In cc
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#define engineCylinders 1 // May support more than 1 cyl later. Always will assume 1 injector per cylinder.
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#define engineInjectorSize 80 // In cc/min
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#define engineStoich 14.7 // Stoichiometric ratio of fuel used
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#define engineStrokes 4 //Can be 2 stroke or 4 stroke, any other value will cause problems
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#define engineDwell 3000 //The spark dwell time in uS
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#define triggerTeeth 12 //The full count of teeth on the trigger wheel if there were no gaps
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#define triggerMissingTeeth 1 //The size of the tooth gap (ie number of missing teeth)
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#define triggerAngle 110 // The angle (Degrees) from TDC that No 1 cylinder is at when tooth #1 passes the sensor. CANNOT BE 0
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//The following lines are configurable, but the defaults are probably pretty good for most applications
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#define engineInjectorDeadTime 1500 //Time in uS that the injector takes to open
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@ -36,8 +28,10 @@ Need to calculate the req_fuel figure here, preferably in pre-processor macro
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#include "fastAnalog.h"
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#include "digitalIOPerformance.h"
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float req_fuel = ((engineCapacity / engineInjectorSize) / engineCylinders / engineStoich) * 100; // This doesn't seem quite correct, but I can't find why. It will be close enough to start an engine
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int req_fuel_uS = req_fuel * 1000; //Convert to uS and, importantly, an int. This is the only variable to be used in calculations
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//NEED TO LOAD FROM EEPROM HERE
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//float req_fuel = ((engineCapacity / engineInjectorSize) / engineCylinders / engineStoich) * 100; // This doesn't seem quite correct, but I can't find why. It will be close enough to start an engine
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int req_fuel_uS = config1.req_fuel * 1000; //Convert to uS and an int. This is the only variable to be used in calculations
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// Setup section
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// These aren't really configuration options, more so a description of how the hardware is setup. These are things that will be defined in the recommended hardware setup
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@ -83,46 +83,47 @@
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; name = array, type, offset, shape, units, scale, translate, lo, hi, digits
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; name = scalar, type, offset, units, scale, translate, lo, hi, digits
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veTable = array, U08, 0, [8x8], "%", 1.0, 0.0, 0.0, 255.0, 0
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crankCold = scalar, U08, 64, "ms", 0.1, 0.0, 0.0, 25.5, 1
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crankHot = scalar, U08, 65, "ms", 0.1, 0.0, 0.0, 25.5, 1
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asePct = scalar, U08, 66, "%", 1.0, 0.0, 0.0, 95.0, 0
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aseCount = scalar, U08, 67, "", 1.0, 0.0, 0.0, 254.0, 0
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wueBins = array, U08, 68, [ 10], "%", 1.0, 0.0, 100.0, 255.0, 0
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taeBins = array, U08, 78, [ 4], "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins1 = scalar, U08, 78, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins2 = scalar, U08, 79, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins3 = scalar, U08, 80, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins4 = scalar, U08, 81, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeColdA = scalar, U08, 82, "ms", 0.1, 0.0, 0.0, 25.5, 1
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tpsThresh = scalar, U08, 83, "v/s",0.1953125, 0.0, 0.2, 49.8, 3
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taeTime = scalar, U08, 84, "ms", 0.1, 0.0, 0.0, 25.5, 1
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tdePct = scalar, U08, 85, "%", 1.0, 0.0, 0.0, 255.0, 0
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#if CELSIUS
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egoTemp = scalar, U08, 86, "°C", 0.555, -72, -40, 102.0, 0
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#else
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egoTemp = scalar, U08, 86, "°F", 1.0, -40, -40, 215.0, 0
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#endif
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egoCount = scalar, U08, 87, "", 1.0, 0.0, 0.0, 255.0, 0
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egoDelta = scalar, U08, 88, "%", 1.0, 0.0, 0.0, 255.0, 0
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egoLimit = scalar, U08, 89, "%", 1.0, 0.0, 0.0, 255.0, 0
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reqFuel = scalar, U08, 90, "ms", 0.1, 0.0, 0.0, 25.5, 1
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divider = scalar, U08, 91, "", 1.0, 0.0
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alternate = bits, U08, 92, [0:0], "Simultaneous", "Alternating"
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injOpen = scalar, U08, 93, "ms", 0.1, 0.0, 0.1, 25.5, 1
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injOCfuel = scalar, U08, 94, "ms", 0.1, 0.0, 0.0, 0.0, 0
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injPwmP = scalar, U08, 95, "%", 1.0, 0.0, 0.0, 100.0, 0
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injPwmT = scalar, U08, 96, "ms", 0.1, 0.0, 0.0, 25.5, 1
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battFac = scalar, U08, 97, "ms/v",0.0166667, 0.0, 0.0, 1.0, 2
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rpmk = scalar, U16, 98, "", 1.0, 0.0
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rpmBins = array, U08, 100, [ 8], "RPM", 100.0, 0.0, 100.0, 25500.0, 0
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rpmBins = array, U08, 64, [ 8], "RPM", 100.0, 0.0, 100.0, 25500.0, 0
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#if SPEED_DENSITY
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mapBins = array, U08, 108, [ 8], "kPa", 1.0, 0.0, 0.0, 255.0, 0
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mapBins = array, U08, 72, [ 8], "kPa", 1.0, 0.0, 0.0, 255.0, 0
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#elif ALPHA_N
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tpsBins = array, U08, 108, [ 8], "TPS", 1.0, 0.0, 0.0, 255.0, 0
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tpsBins = array, U08, 72, [ 8], "TPS", 1.0, 0.0, 0.0, 255.0, 0
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#elif AIR_FLOW_METER
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#error "MSnS does not support MAF"
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#exit
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#endif
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crankCold = scalar, U08, 80, "ms", 0.1, 0.0, 0.0, 25.5, 1
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crankHot = scalar, U08, 81, "ms", 0.1, 0.0, 0.0, 25.5, 1
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asePct = scalar, U08, 82, "%", 1.0, 0.0, 0.0, 95.0, 0
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aseCount = scalar, U08, 83, "", 1.0, 0.0, 0.0, 254.0, 0
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wueBins = array, U08, 84, [ 10], "%", 1.0, 0.0, 100.0, 255.0, 0
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taeBins = array, U08, 94, [ 4], "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins1 = scalar, U08, 94, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins2 = scalar, U08, 95, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins3 = scalar, U08, 96, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeBins4 = scalar, U08, 97, "ms", 0.1, 0.0, 0.0, 25.5, 1
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taeColdA = scalar, U08, 98, "ms", 0.1, 0.0, 0.0, 25.5, 1
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tpsThresh = scalar, U08, 99, "v/s",0.1953125, 0.0, 0.2, 49.8, 3
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taeTime = scalar, U08, 100, "ms", 0.1, 0.0, 0.0, 25.5, 1
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tdePct = scalar, U08, 101, "%", 1.0, 0.0, 0.0, 255.0, 0
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#if CELSIUS
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egoTemp = scalar, U08, 102, "°C", 0.555, -72, -40, 102.0, 0
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#else
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egoTemp = scalar, U08, 102, "°F", 1.0, -40, -40, 215.0, 0
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#endif
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egoCount = scalar, U08, 103, "", 1.0, 0.0, 0.0, 255.0, 0
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egoDelta = scalar, U08, 104, "%", 1.0, 0.0, 0.0, 255.0, 0
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egoLimit = scalar, U08, 105, "%", 1.0, 0.0, 0.0, 255.0, 0
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reqFuel = scalar, U08, 106, "ms", 0.1, 0.0, 0.0, 25.5, 1
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divider = scalar, U08, 107, "", 1.0, 0.0
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alternate = bits, U08, 108, [0:0], "Simultaneous", "Alternating"
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injOpen = scalar, U08, 109, "ms", 0.1, 0.0, 0.1, 25.5, 1
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injOCfuel = scalar, U08, 110, "ms", 0.1, 0.0, 0.0, 0.0, 0
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injPwmP = scalar, U08, 111, "%", 1.0, 0.0, 0.0, 100.0, 0
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injPwmT = scalar, U08, 112, "ms", 0.1, 0.0, 0.0, 25.5, 1
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battFac = scalar, U08, 113, "ms/v",0.0166667, 0.0, 0.0, 1.0, 2
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rpmk = scalar, U16, 114, "", 1.0, 0.0
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; Config1
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mapType = bits, U08, 116, [0:1], "115 kPa", "250 kPa", "INVALID", "INVALID"
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twoStroke = bits, U08, 116, [2:2], "Four-stroke", "Two-stroke"
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@ -148,6 +149,7 @@
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#endif
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egoSwitch = scalar, U08, 122, "v", 0.0196, 0.0, 0.0, 5.0, 3
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taeColdM = scalar, U08, 123, "%", 1.0, 0.0, 0.0, 250.0, 0
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;--------------------------------------------------
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;Start Ignition table (Table 2)
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@ -158,7 +160,7 @@
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rpmBins2 = array, U08, 64,[ 8], "RPM", 100.0, 0.0, 100, 25500, 0
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#if SPEED_DENSITY
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mapBins2 = array, U08, 72, [ 8], "kPa", 1.0, 0.0, 0.0, 255.0, 0
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mapBins2 = array, U08, 72, [ 8], "kPa", 1.0, 0.0, 0.0, 255.0, 0
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#elif ALPHA_N
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tpsBins2 = array, U08, 72, [ 8], "TPS", 1.0, 0.0, 0.0, 255.0, 0
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#elif AIR_FLOW_METER
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@ -166,38 +168,33 @@
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#exit
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#endif
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TrigAng = scalar, U08, 80, "Deg", 0.352, 0, 0, 90, 0
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FixAng = scalar, U08, 81, "Deg", 0.352, -28.4, -10, 80, 0
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Trim = scalar, S08, 82, "Deg", 0.352, 0, -45, 45, 0
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CrankAng = scalar, U08, 83, "Deg", 0.352, -28.4, -10, 80, 0
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IgHold = scalar, U08, 84, "", 1, 0, 0, 100, 0
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Trig_plus = bits, U08, 85[0:1], "0", "+22.5", "INVALID", "+45"
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TrigCrank = bits, U08, 85[2:2], "Trigger Return", "Time Based"
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IgInv = bits, U08, 85[3:3], "No", "Yes"
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oddfire = bits, U08, 85[4:4], "No", "Yes"
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IdleAdv = scalar, U08, 86, "Deg", 0.352,-28.4, -10, 80, 0
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IdleAdvTPS = scalar, U08, 87, "ADC", 1, 0, 0, 255, 0
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IdleAdvRPM = scalar, U08, 88, "RPM", 100, 0, 0, 1200, 0
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TrigAng = scalar, U08, 80, "Deg", 0.352, 0, 0, 90, 0
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FixAng = scalar, U08, 81, "Deg", 0.352, -28.4, -10, 80, 0
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Trim = scalar, S08, 82, "Deg", 0.352, 0, -45, 45, 0
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CrankAng = scalar, U08, 83, "Deg", 0.352, -28.4, -10, 80, 0
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IgHold = scalar, U08, 84, "", 1, 0, 0, 100, 0
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Trig_plus = bits, U08, 85[0:1], "0", "+22.5", "INVALID", "+45"
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TrigCrank = bits, U08, 85[2:2], "Trigger Return", "Time Based"
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IgInv = bits, U08, 85[3:3], "No", "Yes"
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oddfire = bits, U08, 85[4:4], "No", "Yes"
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IdleAdv = scalar, U08, 86, "Deg", 0.352,-28.4, -10, 80, 0
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IdleAdvTPS = scalar, U08, 87, "ADC", 1, 0, 0, 255, 0
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IdleAdvRPM = scalar, U08, 88, "RPM", 100, 0, 0, 1200, 0
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#if CELSIUS
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IdleAdvCLT = scalar, U08, 89, "C", 0.555, -72, -40, 102, 1
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IdleAdvCLT = scalar, U08, 89, "C", 0.555, -72, -40, 102, 1
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#else
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IdleAdvCLT = scalar, U08, 89, "F", 1, -40, -40, 215, 0
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IdleAdvCLT = scalar, U08, 89, "F", 1, -40, -40, 215, 0
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#endif
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IdleDelayTime = scalar, U08, 90, "sec", 1, 0, 0, 5, 0
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||||
StgCycles = scalar, U08, 91, "cycles", 1, 0, 0, 255, 0
|
||||
#if MPXH6300A
|
||||
Stg2ndParmKPA = scalar, U08, 92, "KPa", 1.213675, 1.53, 0, 304.0, 0
|
||||
Stg2ndParmDlt = scalar, U08, 93, "KPa", 1.213675, 1.53, 0, 304.0, 0
|
||||
#elif MPXH6400A
|
||||
Stg2ndParmKPA = scalar, U08, 92, "KPa", 1.6197783, 2.147, 20.0, 400.0, 0
|
||||
Stg2ndParmDlt = scalar, U08, 93, "KPa", 1.6197783, 2.147, 20.0, 400.0, 0
|
||||
#else
|
||||
Stg2ndParmKPA = scalar, U08, 92, "kPa", 1, 0, 0, 255, 0
|
||||
Stg2ndParmDlt = scalar, U08, 93, "kPa", 1,0,0,255,0
|
||||
#endif
|
||||
spare2_94 = scalar, U08, 94, "", 1, 0, 0, 255, 0
|
||||
spare2_95 = scalar, U08, 95, "", 1, 0, 0, 255, 0
|
||||
spare2_96 = scalar, U08, 96, "", 1, 0, 0, 255, 0
|
||||
IdleDelayTime = scalar, U08, 90, "sec", 1, 0, 0, 5, 0
|
||||
StgCycles = scalar, U08, 91, "cycles", 1, 0, 0, 255, 0
|
||||
|
||||
;Dwell control
|
||||
;running dwell variable railed to 8 - who needs more than 8ms?
|
||||
dwellcont = bits, U08, 92, [1:1], "Fixed duty*^", "Dwell control"
|
||||
dwellcrank = scalar, U08, 93, "ms", 0.1, 0, 0, 25, 1
|
||||
dwellrun = scalar, U08, 94, "ms", 0.1, 0, 0, 8, 1
|
||||
triggerTeeth = scalar, U08, 95, "teeth", 1.0, 0.0, 0.0, 255, 0 ; * ( 1 byte)
|
||||
No_Miss_Teeth = scalar, U08, 96, "teeth", 1.0, 0.0, 0.0, 255, 0 ; * ( 1 byte )
|
||||
|
||||
;-------------------------------------------------------------------------------
|
||||
|
||||
|
|
|
|||
|
|
@ -0,0 +1,23 @@
|
|||
#include <EEPROM.h>
|
||||
|
||||
void writeConfig();
|
||||
void writeTables();
|
||||
|
||||
void loadConfig();
|
||||
void loadTables();
|
||||
|
||||
/*
|
||||
Current layout of data (Version 1) is as follows (All sizes are in bytes):
|
||||
|---------------------------------------------------|
|
||||
|Byte # |Size | Description |
|
||||
|---------------------------------------------------|
|
||||
| 0 |1 | Data structure version |
|
||||
| 1 |2 | X and Y sizes for VE table |
|
||||
| 3 |125 | Config Page 1 (VE Table) |
|
||||
| 128 |2 | X and Y sizes for Ign table |
|
||||
| 130 |125 | Config Page 2 (Ign Table) |
|
||||
-----------------------------------------------------
|
||||
*/
|
||||
|
||||
#define EEPROM_CONFIG1 3
|
||||
#define EEPROM_CONFIG2 130
|
||||
|
|
@ -0,0 +1,2 @@
|
|||
|
||||
|
||||
4
table.h
4
table.h
|
|
@ -4,8 +4,8 @@ This file is used for everything related to maps/tables including their definiti
|
|||
#include <Arduino.h>
|
||||
struct table {
|
||||
//All tables must be the same size for simplicity
|
||||
const static int xSize = 8;
|
||||
const static int ySize = 8;
|
||||
const static byte xSize = 8;
|
||||
const static byte ySize = 8;
|
||||
|
||||
byte values[ySize][xSize];
|
||||
int axisX[xSize];
|
||||
|
|
|
|||
Loading…
Reference in New Issue