wow Leiderman-Khlystov
This commit is contained in:
Andrey
parent
4c9df01b64
commit
4d65067345
|
|
@ -0,0 +1,117 @@
|
|||
#include "pch.h"
|
||||
#include "rusefi_lua.h"
|
||||
#include "lua_lib.h"
|
||||
|
||||
|
||||
// Leiderman-Khlystov Coefficients for Estimating Engine Full Load Characteristics and Performance
|
||||
TEST(LuaVag, LeidermaKhlystov) {
|
||||
const char* magic = LUA_POW R"(
|
||||
|
||||
|
||||
currentRpm = 2000
|
||||
|
||||
maxPowerHp = 148
|
||||
maxPowerRpm = 6000
|
||||
maxTorqueNm = 147
|
||||
maxTorqueRpm = 3500
|
||||
|
||||
|
||||
maxPowerKw = maxPowerHp * 0.7355
|
||||
|
||||
|
||||
torqAtMaxPower = maxPowerKw * 9549 / maxPowerRpm
|
||||
print('torqAtMaxPower ' ..torqAtMaxPower)
|
||||
|
||||
rpmCoef = maxPowerRpm / maxTorqueRpm
|
||||
print('rpmCoef ' ..rpmCoef)
|
||||
|
||||
torqCoef = maxTorqueNm / torqAtMaxPower
|
||||
print('torqCoef ' ..torqCoef)
|
||||
|
||||
torquePotential =(torqCoef -1) * 100
|
||||
zz =(100 *(rpmCoef -1) *(rpmCoef -1))
|
||||
print('torquePotential ' ..torquePotential)
|
||||
print('zz ' ..zz)
|
||||
|
||||
ax = 1 -((torquePotential * rpmCoef *(2 - rpmCoef)) / zz)
|
||||
bx = 2 *((torquePotential * rpmCoef) / zz)
|
||||
cx =(torquePotential * rpmCoef * rpmCoef) / zz
|
||||
|
||||
print('ax ' ..ax .. ', bx ' ..bx .. ', cx ' ..cx)
|
||||
|
||||
rpmRatio = currentRpm / maxPowerRpm
|
||||
abcMult = ax * rpmRatio + bx * pow(rpmRatio, 2) - cx * pow(rpmRatio, 3)
|
||||
print ('abcMult ' ..abcMult)
|
||||
|
||||
print('rpmRatio ' .. rpmRatio)
|
||||
|
||||
LeidermanPower = maxPowerKw * abcMult
|
||||
print('LeidermanPower ' .. LeidermanPower)
|
||||
|
||||
LeidermanTorque = (9550 * LeidermanPower) / currentRpm
|
||||
print('LeidermanTorque ' .. LeidermanTorque)
|
||||
|
||||
function testFunc()
|
||||
return LeidermanTorque
|
||||
end
|
||||
|
||||
)";
|
||||
|
||||
EXPECT_NEAR_M3(testLuaReturnsNumberOrNil(magic).value_or(0), 156.463);
|
||||
}
|
||||
|
||||
|
||||
TEST(LuaVag, LeidermaKhlystov2) {
|
||||
const char* magic = LUA_POW R"(
|
||||
|
||||
|
||||
currentRpm = 2000
|
||||
|
||||
maxPowerHp = 148
|
||||
maxPowerRpm = 6000
|
||||
maxTorqueNm = 147
|
||||
maxTorqueRpm = 3500
|
||||
|
||||
|
||||
maxPowerKw = maxPowerHp * 0.7355
|
||||
|
||||
|
||||
torqAtMaxPower = maxPowerKw * 9549 / maxPowerRpm
|
||||
print('torqAtMaxPower ' ..torqAtMaxPower)
|
||||
|
||||
rpmCoef = maxPowerRpm / maxTorqueRpm
|
||||
print('rpmCoef ' ..rpmCoef)
|
||||
|
||||
torqCoef = maxTorqueNm / torqAtMaxPower
|
||||
print('torqCoef ' ..torqCoef)
|
||||
|
||||
torquePotential =(torqCoef -1) * 100
|
||||
|
||||
print('torquePotential ' ..torquePotential)
|
||||
|
||||
ax=2-(25/torquePotential);
|
||||
bx=(50/torquePotential) - 1;
|
||||
cx=25/torquePotential;
|
||||
|
||||
print('ax ' ..ax .. ', bx ' ..bx .. ', cx ' ..cx)
|
||||
|
||||
rpmRatio = currentRpm / maxPowerRpm
|
||||
abcMult = ax * rpmRatio + bx * pow(rpmRatio, 2) - cx * pow(rpmRatio, 3)
|
||||
print ('abcMult ' ..abcMult)
|
||||
|
||||
print('rpmRatio ' .. rpmRatio)
|
||||
|
||||
LeidermanPower = maxPowerKw * abcMult
|
||||
print('LeidermanPower ' .. LeidermanPower)
|
||||
|
||||
LeidermanTorque = (9550 * LeidermanPower) / currentRpm
|
||||
print('LeidermanTorque ' .. LeidermanTorque)
|
||||
|
||||
function testFunc()
|
||||
return LeidermanTorque
|
||||
end
|
||||
|
||||
)";
|
||||
|
||||
EXPECT_NEAR_M3(testLuaReturnsNumberOrNil(magic).value_or(0), 415.858);
|
||||
}
|
||||
|
|
@ -261,61 +261,3 @@ TEST(LuaVag, ChecksumMotor6) {
|
|||
|
||||
EXPECT_NEAR_M3(testLuaReturnsNumberOrNil(realdata).value_or(0), 0x3D);
|
||||
}
|
||||
|
||||
|
||||
// Leiderman-Khlystov Coefficients for Estimating Engine Full Load Characteristics and Performance
|
||||
TEST(LuaVag, LeidermaKhlystov) {
|
||||
const char* magic = LUA_POW VAG_CHECKSUM realMotor6Packet R"(
|
||||
|
||||
|
||||
currentRpm = 2000
|
||||
|
||||
maxPowerHp = 148
|
||||
maxPowerRpm = 6000
|
||||
maxTorqueNm = 147
|
||||
maxTorqueRpm = 3500
|
||||
|
||||
|
||||
maxPowerKw = maxPowerHp * 0.7355
|
||||
|
||||
|
||||
torqAtMaxPower = maxPowerKw * 9549 / maxPowerRpm
|
||||
print('torqAtMaxPower ' ..torqAtMaxPower)
|
||||
|
||||
rpmCoef = maxPowerRpm / maxTorqueRpm
|
||||
print('rpmCoef ' ..rpmCoef)
|
||||
|
||||
torqCoef = maxTorqueNm / torqAtMaxPower
|
||||
print('torqCoef ' ..torqCoef)
|
||||
|
||||
torquePotential =(torqCoef -1) * 100
|
||||
zz =(100 *(rpmCoef -1) *(rpmCoef -1))
|
||||
print('torquePotential ' ..torquePotential)
|
||||
print('zz ' ..zz)
|
||||
|
||||
ax = 1 -((torquePotential * rpmCoef *(2 - rpmCoef)) / zz)
|
||||
bx = 2 *((torquePotential * rpmCoef) / zz)
|
||||
cx =(torquePotential * rpmCoef * rpmCoef) / zz
|
||||
|
||||
print('ax ' ..ax .. ', bx ' ..bx .. ', cx ' ..cx)
|
||||
|
||||
rpmRatio = currentRpm / maxPowerRpm
|
||||
abcMult = ax * rpmRatio + bx * pow(rpmRatio, 2) - cx * pow(rpmRatio, 3)
|
||||
print ('abcMult ' ..abcMult)
|
||||
|
||||
print('rpmRatio ' .. rpmRatio)
|
||||
|
||||
LeidermanPower = maxPowerKw * abcMult
|
||||
print('LeidermanPower ' .. LeidermanPower)
|
||||
|
||||
LeidermanTorque = (9550 * LeidermanPower) / currentRpm
|
||||
print('LeidermanTorque ' .. LeidermanTorque)
|
||||
|
||||
function testFunc()
|
||||
return LeidermanTorque
|
||||
end
|
||||
|
||||
)";
|
||||
|
||||
EXPECT_NEAR_M3(testLuaReturnsNumberOrNil(magic).value_or(0), 156.463);
|
||||
}
|
||||
|
|
|
|||
|
|
@ -37,6 +37,7 @@ TESTS_SRC_CPP = \
|
|||
tests/lua/test_lua_vag.cpp \
|
||||
tests/lua/test_lua_with_engine.cpp \
|
||||
tests/lua/test_lua_hooks.cpp \
|
||||
tests/lua/test_lua_Leiderman_Khlystov.cpp \
|
||||
tests/lua/test_can_filter.cpp \
|
||||
tests/sensor/test_cj125.cpp \
|
||||
tests/test_change_engine_type.cpp \
|
||||
|
|
|
|||
Loading…
Reference in New Issue