mirror of https://github.com/rusefi/rusefi-1.git
37 lines
1.3 KiB
C
37 lines
1.3 KiB
C
/**
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* @file fuel_math.h
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*
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* @date May 27, 2013
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* @author Andrey Belomutskiy, (c) 2012-2020
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*/
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#pragma once
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#include "engine_ptr.h"
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#include "rusefi_types.h"
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void initFuelMap(DECLARE_ENGINE_PARAMETER_SIGNATURE);
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/**
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* @return baseFuel with CLT and IAT corrections
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*/
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floatms_t getRunningFuel(floatms_t baseFuel DECLARE_ENGINE_PARAMETER_SUFFIX);
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float getBaroCorrection(DECLARE_ENGINE_PARAMETER_SIGNATURE);
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int getNumberOfInjections(injection_mode_e mode DECLARE_ENGINE_PARAMETER_SUFFIX);
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angle_t getInjectionOffset(float rpm, float load DECLARE_ENGINE_PARAMETER_SUFFIX);
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float getIatFuelCorrection(DECLARE_ENGINE_PARAMETER_SIGNATURE);
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float getCltFuelCorrection(DECLARE_ENGINE_PARAMETER_SIGNATURE);
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float getFuelCutOffCorrection(efitick_t nowNt, int rpm DECLARE_ENGINE_PARAMETER_SUFFIX);
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angle_t getCltTimingCorrection(DECLARE_ENGINE_PARAMETER_SIGNATURE);
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float getCrankingFuel(float baseFuel DECLARE_ENGINE_PARAMETER_SUFFIX);
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float getCrankingFuel3(float baseFuel, uint32_t revolutionCounterSinceStart DECLARE_ENGINE_PARAMETER_SUFFIX);
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floatms_t getInjectionMass(int rpm DECLARE_ENGINE_PARAMETER_SUFFIX);
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percent_t getInjectorDutyCycle(int rpm DECLARE_ENGINE_PARAMETER_SUFFIX);
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float getStandardAirCharge(DECLARE_ENGINE_PARAMETER_SIGNATURE);
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struct AirmassModelBase;
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AirmassModelBase* getAirmassModel(engine_load_mode_e mode DECLARE_ENGINE_PARAMETER_SUFFIX);
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