rusefi/firmware/controllers/algo/advance_map.cpp

/**
 * @file	advance_map.cpp
 *
 * @date Mar 27, 2013
 * @author Andrey Belomutskiy, (c) 2012-2015
 *
 * This file is part of rusEfi - see http://rusefi.com
 *
 * rusEfi is free software; you can redistribute it and/or modify it under the terms of
 * the GNU General Public License as published by the Free Software Foundation; either
 * version 3 of the License, or (at your option) any later version.
 *
 * rusEfi is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without
 * even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
 * GNU General Public License for more details.
 *
 * You should have received a copy of the GNU General Public License along with this program.
 * If not, see <http://www.gnu.org/licenses/>.
 */

#include "main.h"
#include "advance_map.h"
#include "interpolation.h"
#include "efilib2.h"
#include "engine_configuration.h"
#include "engine_math.h"

EXTERN_ENGINE;

static ign_Map3D_t advanceMap("advance");
static ign_Map3D_t iatAdvanceCorrectionMap("iat corr");

static const float iatTimingRpmBins[IGN_LOAD_COUNT] = {880,	1260,	1640,	2020,	2400,	2780,	3000,	3380,	3760,	4140,	4520,	5000,	5700,	6500,	7200,	8000};

//880	1260	1640	2020	2400	2780	3000	3380	3760	4140	4520	5000	5700	6500	7200	8000
static const ignition_table_t defaultIatTiming = {
		{ 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 2, 2, 2, 2, 2},
		{ 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 2, 2, 2, 2, 2},
		{ 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 2, 2, 2, 2, 2},
		{ 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 4, 2, 2, 2, 2, 2},
		{3.5, 3.5, 3.5, 3.5, 3.5, 3.5, 3.5, 3.5, 3.5, 3.5, 3.5, 2, 2, 2, 2, 2},
		{ 3, 3, 3, 3, 3, 3, 3, 3, 3, 3, 3, 2, 2, 2, 2, 2},
		{ 2, 2, 2, 2, 2, 2, 2, 2, 2, 2, 2, 0, 0, 0, 0, 0},
		{ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0},
		{ 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0},
		{ 0, 0, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9, -0.9},
		{ -3.3, -3.4, -4.9, -4.9, -4.9, -4.9, -4.4, -4.4, -4.4, -4.4, -4.4, -0.9, -0.9, -0.9, -0.9, -0.9},
		{ -4.4, -4.9, -5.9, -5.9, -5.9, -5.9, -4.9, -4.9, -4.9, -4.9, -4.9, -2.4, -2.4, -2.4, -2.4, -2.4},
		{ -4.4, -4.9, -5.9, -5.9, -5.9, -5.9, -4.9, -4.9, -4.9, -4.9, -4.9, -2.9, -2.9, -2.9, -2.9, -2.9},
		{-4.4, -4.9, -5.9, -5.9, -5.9, -5.9, -4.9, -4.9, -4.9, -4.9, -4.9, -3.9, -3.9, -3.9, -3.9, -3.9},
		{-4.4, -4.9, -5.9, -5.9, -5.9, -5.9, -4.9, -4.9, -4.9, -4.9, -4.9, -3.9, -3.9, -3.9, -3.9, -3.9},
		{-4.4, -4.9, -5.9, -5.9, -5.9, -5.9, -4.9, -4.9, -4.9, -4.9, -4.9, -3.9, -3.9, -3.9, -3.9, -3.9},
};

bool_t isStep1Condition(int rpm DECLARE_ENGINE_PARAMETER_S) {
	return  boardConfiguration->enabledStep1Limiter && rpm >= engineConfiguration->step1rpm;
}

/**
 * @return ignition timing angle advance before TDC
 */
static angle_t getRunningAdvance(int rpm, float engineLoad DECLARE_ENGINE_PARAMETER_S) {
	engine->m.beforeAdvance = GET_TIMESTAMP();
	if (cisnan(engineLoad)) {
		warning(OBD_PCM_Processor_Fault, "NaN engine load");
		return NAN;
	}
	efiAssert(!cisnan(engineLoad), "invalid el", NAN);
	efiAssert(!cisnan(engineLoad), "invalid rpm", NAN);
	engine->m.beforeZeroTest = GET_TIMESTAMP();
	engine->m.zeroTestTime = GET_TIMESTAMP() - engine->m.beforeZeroTest;

	if (isStep1Condition(rpm PASS_ENGINE_PARAMETER)) {
		return engineConfiguration->step1timing;
	}

	float iatCorrection = iatAdvanceCorrectionMap.getValue(engine->engineState.iat, (float) rpm);

	float result = advanceMap.getValue(engineLoad, (float) rpm) + iatCorrection
			// todo: uncomment once we get useable knock   - engine->knockCount
			;
	engine->m.advanceLookupTime = GET_TIMESTAMP() - engine->m.beforeAdvance;
	return result;
}

angle_t getAdvance(int rpm, float engineLoad DECLARE_ENGINE_PARAMETER_S) {
	angle_t angle;
	if (isCrankingR(rpm)) {
		angle = engineConfiguration->crankingTimingAngle;
	} else {
		angle = getRunningAdvance(rpm, engineLoad PASS_ENGINE_PARAMETER);
	}
	angle -= engineConfiguration->ignitionOffset;
	fixAngle(angle);
	return angle;
}

void setDefaultIatTimingCorrection(DECLARE_ENGINE_PARAMETER_F) {
	setTableBin2(config->ignitionIatCorrLoadBins, IGN_LOAD_COUNT, -40, 110, 1);
	memcpy(config->ignitionIatCorrRpmBins, iatTimingRpmBins, sizeof(iatTimingRpmBins));
	copyTimingTable(defaultIatTiming, config->ignitionIatCorrTable);
}

void prepareTimingMap(DECLARE_ENGINE_PARAMETER_F) {
	advanceMap.init(config->ignitionTable, config->ignitionLoadBins,
			config->ignitionRpmBins);
	iatAdvanceCorrectionMap.init(config->ignitionIatCorrTable, config->ignitionIatCorrLoadBins,
			config->ignitionIatCorrRpmBins);
}

/**
 * @param octane gas octane number
 * @param bore in mm
 */
float getTopAdvanceForBore(chamber_style_e style, int octane, double compression, double bore) {
    int octaneCorrection;
    if ( octane <= 90) {
        octaneCorrection = -2;
    } else if (octane < 94) {
        octaneCorrection = -1;
    } else {
        octaneCorrection = 0;
    }

    int compressionCorrection;
    if (compression <= 9) {
        compressionCorrection = 2;
    } else if (compression <= 10) {
        compressionCorrection = 1;
    } else if (compression <= 11) {
        compressionCorrection = 0;
    } else {
        // compression ratio above 11
        compressionCorrection = -2;
    }
    int base;
    if (style == CS_OPEN) {
    	base = 33;
    } else if (style == CS_CLOSED) {
    	base = 28;
    } else {
    	// CS_SWIRL_TUMBLE
    	base = 22;
    }

    float boreCorrection = (bore - 4 * 25.4) / 25.4 * 6;
    float result = base + octaneCorrection + compressionCorrection + boreCorrection;
    return ((int)(result * 10)) / 10.0;
}