Mapped CI Engine

Compression-ignition engine model using lookup tables

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Libraries:
Powertrain Blockset / Propulsion / Combustion Engines
Vehicle Dynamics Blockset / Powertrain / Propulsion

Description

The Mapped CI Engine block implements a mapped compression-ignition (CI) engine model using power, air mass flow, fuel flow, exhaust temperature, efficiency, and emission performance lookup tables. You can use the block for:

• Hardware-in-the-loop (HIL) engine control design

• Vehicle-level fuel economy and performance simulations

The lookup tables, developed with the Model-Based Calibration Toolbox™, are functions of injected fuel mass, F, engine torque, T, engine speed, N, and engine temperature, Temp_Eng.

Input Command Setting	Input Engine Temperature Parameter Setting	Lookup Tables
Fuel mass	off	ƒ(F,N)
	on	ƒ(F,N,TempEng)
Torque	off	ƒ(T,N)
	on	ƒ(T,N,TempEng)

The block enables you to specify lookup tables for these engine characteristics:

• Power

• Air

• Fuel

• Temperature

• Efficiency

• Hydrocarbon (HC) emissions

• Carbon monoxide (CO) emissions

• Nitric oxide and nitrogen dioxide (NOx) emissions

• Carbon dioxide (CO₂) emissions

• Particulate matter (PM) emissions

To bound the Mapped CI Engine block output, the block does not extrapolate the lookup table data.

Virtual Calibration

If you have Model-Based Calibration Toolbox, click Calibrate Maps to virtually calibrate the 2D lookup tables using measured data. The dialog box steps through these tasks.

Task	Description
Import firing data	Import this loss data from a file. For example, open <matlabroot>/toolbox/mbc/mbctraining/CiEngineData.xlsx. For more information, see Using Data (Model-Based Calibration Toolbox). Input command Required Data Optional Data Fuel mass Engine speed, rpm Commanded fuel mass per injection, mg Engine torque, N·m Air mass flow rate, kg/s Brake specific fuel consumption, g/(kW·h) CO2 mass flow rate, kg/s CO mass flow rate, kg/s Exhaust temperature, K Fuel mass flow rate, kg/s HC mass flow rate, kg/s NOx mass flow rate, kg/s Particulate matter mass flow rate, kg/s Torque Engine speed, rpm Engine torque, N·m Collect firing data at steady-state operating conditions when injectors deliver the fuel. Data should cover the engine speed and torque operating range. Model-Based Calibration Toolbox uses the firing data boundary as the maximum torque. To filter or edit the data, select Edit in Application. The Model-Based Calibration Toolbox Data Editor opens.
Import non-firing data	Import this non-firing data from a file. For example, open <matlabroot>/toolbox/mbc/mbctraining/CiEngineData.xlsx. Engine speed, rpm Engine torque, N·m Collect non-firing (motoring) data at steady-state operating conditions when fuel is cut off. All non-firing torque points must be less than zero. Non-firing data is a function of engine speed only.
Generate response models	For both firing and non-firing data, the Model-Based Calibration Toolbox uses test plans to fit data to Gaussian process models (GPMs). To assess or adjust the response model fit, select Edit in Application. The Model-Based Calibration Toolbox Model Browser opens. For more information, see Model Assessment (Model-Based Calibration Toolbox).
Generate calibration	Model-Based Calibration Toolbox calibrates the firing and non-firing response models and generates calibrated tables. To assess or adjust the calibration, select Edit in Application. The Model-Based Calibration Toolbox CAGE Browser opens. For more information, see Calibration Lookup Tables (Model-Based Calibration Toolbox).
Update block parameters	Update the block lookup table and breakpoint parameters with the calibration.

Cylinder Air Mass

The block calculates the normalized cylinder air mass using these equations.

$$\begin{array}{l}{M}_{Nom}=\frac{P_{std}{V}_d}{N_{cyl}{R}_{air}{T}_{std}}\\ L=\frac{\left(\frac{60s}{min}\right)Cps\cdot {\dot{m}}_{air}}{\left(\frac{1000g}{Kg}\right)N_{cyl}\cdot N\cdot M_{Nom}}\end{array}$$

The equations use these variables.

L	Normalized cylinder air mass
$M_{Nom}$	Nominal engine cylinder air mass at standard temperature and pressure, piston at bottom dead center (BDC) maximum volume, in kg
$$Cps$$	Crankshaft revolutions per power stroke, rev/stroke
$P_{std}$	Standard pressure
$T_{std}$	Standard temperature
$R_{air}$	Ideal gas constant for air and burned gas mixture
$V_d$	Displaced volume
$N_{cyl}$	Number of engine cylinders
N	Engine speed
${\dot{m}}_{intk}$	Engine air mass flow, in g/s

Turbocharger Lag

To model turbocharger lag, select Include turbocharger lag effect. Turbocharger lag limits the maximum fuel mass per injection. To model the maximum fuel mass per injection, the block uses a first-order system with a time constant. At low torque, the engine does not require boost to provide sufficient air flow. When the requested fuel mass requires boost, the block uses a time constant to determine the maximum fuel mass per injection. The block uses these equations for the specified Input command setting.

Calculation	Input command Parameter Setting
	Fuel mass	Torque
Dynamic torque	$$\frac{d{F}_{max}}{dt}=\frac{1}{{\tau }_{eng}}(F_{cmd}-F_{max})$$	$$\frac{d{T}_{max}}{dt}=\frac{1}{{\tau }_{eng}}(T_{cmd}-T_{max})$$
Fuel mass per injection or torque - with turbocharger lag	$$F=\{\begin{array}{c}{F}_{cmd}\text{ when }{F}_{cmd}<F_{\max }\\ F_{max}\text{ when }{F}_{cmd}\ge F_{\max }\end{array}$$	$$T_{target}=\{\begin{array}{c}{T}_{cmd}\text{ when }{T}_{cmd}<T_{\max }\\ T_{max}\text{ when }{T}_{cmd}\ge T_{\max }\end{array}$$
Fuel mass per injection or torque- without turbocharger lag	$$F=F_{cmd}=F_{max}$$	$$T_{target}=T_{cmd}=T_{max}$$
Boost time constant	$${\tau }_{bst}=\{\begin{array}{c}{\tau }_{bst,rising}\text{ when }{F}_{cmd}>F_{\max }\\ {\tau }_{bst,falling}\text{ when }{F}_{cmd}\le F_{\max }\end{array}$$	$${\tau }_{bst}=\{\begin{array}{c}{\tau }_{bst,rising}\text{ when }{T}_{cmd}>T_{\max }\\ {\tau }_{bst,falling}\text{ when }{T}_{cmd}\le T_{\max }\end{array}$$
Final time constant	$${\tau }_{eng}=\{\begin{array}{c}{\tau }_{nat}\text{ when }{T}_{brake}<f_{bst}(N)\\ {\tau }_{bst}\text{ when }{T}_{brake}\ge f_{bst}(N)\end{array}$$

The equations use these variables.

Tbrake	Brake torque
F	Fuel mass per injection
Fcmd, Fmax	Commanded and maximum fuel mass per injection, respectively
Ttarget, Tcmd, Tmax	Target, commanded, and maximum torque, respectively
τbst	Boost time constant
τbst,rising, τbst,falling	Boost rising and falling time constant, respectively
τeng	Final time constant
τnat	Time constant below the boost torque speed line
ƒbst(N)	Boost torque/speed line
N	Engine speed

Fuel Flow

To calculate the fuel economy for high-fidelity models, the block uses the volumetric fuel flow.

$$Q_{fuel}=\frac{{\dot{m}}_{fuel}}{\left(\frac{1000kg}{m^3}\right)S{g}_{fuel}}$$

The equation uses these variables.

$${\dot{m}}_{fuel}$$	Fuel mass flow
Sgfuel	Specific gravity of fuel
Qfuel	Volumetric fuel flow

Power Accounting

For the power accounting, the block implements these equations.

Bus Signal			Description	Equations
PwrInfo	PwrTrnsfrd — Power transferred between blocks Positive signals indicate flow into block Negative signals indicate flow out of block	PwrCrkshft	Crankshaft power	$-{\tau }_{eng}\omega$
	PwrNotTrnsfrd — Power crossing the block boundary, but not transferred Positive signals indicate an input Negative signals indicate a loss	PwrFuel	Fuel input power	${\dot{m}}_{fuel}LHV$
		PwrLoss	Power loss	${\tau }_{eng}\omega -{\dot{m}}_{fuel}LHV$
	PwrStored — Stored energy rate of change Positive signals indicate an increase Negative signals indicate a decrease		Not used

The equations use these variables.

LHV	Fuel lower heating value
ω	Engine speed, rad/s
$${\dot{m}}_{fuel}$$	Fuel mass flow
τeng	Fuel mass per injection time constant

Examples

CI Engine Dynamometer Reference Application

Simulate a compression-ignition (CI) engine and controller under a dynamometer test harness using the CI engine dynamometer reference application.

• Open Script

Ports

Input

FuelMassCmd — Injected fuel mass command

scalar

Injected fuel mass command, F, in mg/inj.

Dependencies

To enable this port, for Input command, select Fuel mass.

TrqCmd — Torque command

scalar

Torque command, T, in N·m.

Dependencies

To enable this port, for Input command, select Torque.

EngSpd — Engine speed

scalar

Engine speed, N, in rpm.

EngTemp — Engine temperature

scalar

Engine temperature, Temp_Eng, in K.

Dependencies

To enable this port, select Input engine temperature.

Output

Info — Bus signal

bus

Bus signal containing these block calculations.

Signal			Description	Units
IntkGasMassFlw			Engine air mass flow output	kg/s
NrmlzdAirChrg			Normalized engine cylinder air mass	N/A
Afr			Air-fuel ratio (AFR)	N/A
FuelMassFlw			Engine fuel flow output	kg/s
FuelVolFlw			Volumetric fuel flow	m3/s
ExhManGasTemp			Engine exhaust gas temperature	K
EngTrq			Engine torque output	N·m
EngSpd			Engine speed	rpm
CrkAng			Engine crankshaft absolute angle $${\displaystyle \underset{0}{\overset{(360)Cps}{\int }}EngSpd\frac{180}{30}d\theta }$$ where $$Cps$$ is crankshaft revolutions per power stroke.	degrees crank angle
Bsfc			Engine brake-specific fuel consumption (BSFC)	g/kWh
EoHC			Engine out hydrocarbon emission mass flow	kg/s
EoCO			Engine out carbon monoxide emission mass flow rate	kg/s
EoNOx			Engine out nitric oxide and nitrogen dioxide emissions mass flow	kg/s
EoCO2			Engine out carbon dioxide emission mass flow	kg/s
EoPM			Engine out particulate matter emission mass flow	kg/s
PwrInfo	PwrTrnsfrd	PwrCrkshft	Crankshaft power	W
	PwrNotTrnsfrd	PwrFuel	Fuel input power	W
		PwrLoss	Power loss	W
	PwrStored		Not used

EngTrq — Power

scalar

Engine power, $T_{brake}$, in N·m.

Parameters

Block Options

Input command — Table functions

Fuel mass (default) | Torque

The lookup tables, developed with the Model-Based Calibration Toolbox, are functions of injected fuel mass, F, engine torque, T, engine speed, N, and engine temperature, Temp_Eng.

Input Command Setting	Input Engine Temperature Parameter Setting	Lookup Tables
Fuel mass	off	ƒ(F,N)
	on	ƒ(F,N,TempEng)
Torque	off	ƒ(T,N)
	on	ƒ(T,N,TempEng)

Dependencies

• Selecting Fuel mass enables Breakpoints for commanded fuel mass input, f_tbrake_f_bpt.

• Selecting Torque enables Breakpoints for commanded torque input, f_tbrake_t_bpt.

• Selecting Input engine temperature enables Breakpoints for temperature input, f_tbrake_engtmp_bpt.

Include turbocharger lag effect — Increase time constant

off (default)

To model turbocharger lag, select Include turbocharger lag effect. Turbocharger lag limits the maximum fuel mass per injection. To model the maximum fuel mass per injection, the block uses a first-order system with a time constant. At low torque, the engine does not require boost to provide sufficient air flow. When the requested fuel mass requires boost, the block uses a time constant to determine the maximum fuel mass per injection. The block uses these equations for the specified Input command setting.

Calculation	Input command Parameter Setting
	Fuel mass	Torque
Dynamic torque	$$\frac{d{F}_{max}}{dt}=\frac{1}{{\tau }_{eng}}(F_{cmd}-F_{max})$$	$$\frac{d{T}_{max}}{dt}=\frac{1}{{\tau }_{eng}}(T_{cmd}-T_{max})$$
Fuel mass per injection or torque - with turbocharger lag	$$F=\{\begin{array}{c}{F}_{cmd}\text{ when }{F}_{cmd}<F_{\max }\\ F_{max}\text{ when }{F}_{cmd}\ge F_{\max }\end{array}$$	$$T_{target}=\{\begin{array}{c}{T}_{cmd}\text{ when }{T}_{cmd}<T_{\max }\\ T_{max}\text{ when }{T}_{cmd}\ge T_{\max }\end{array}$$
Fuel mass per injection or torque- without turbocharger lag	$$F=F_{cmd}=F_{max}$$	$$T_{target}=T_{cmd}=T_{max}$$
Boost time constant	$${\tau }_{bst}=\{\begin{array}{c}{\tau }_{bst,rising}\text{ when }{F}_{cmd}>F_{\max }\\ {\tau }_{bst,falling}\text{ when }{F}_{cmd}\le F_{\max }\end{array}$$	$${\tau }_{bst}=\{\begin{array}{c}{\tau }_{bst,rising}\text{ when }{T}_{cmd}>T_{\max }\\ {\tau }_{bst,falling}\text{ when }{T}_{cmd}\le T_{\max }\end{array}$$
Final time constant	$${\tau }_{eng}=\{\begin{array}{c}{\tau }_{nat}\text{ when }{T}_{brake}<f_{bst}(N)\\ {\tau }_{bst}\text{ when }{T}_{brake}\ge f_{bst}(N)\end{array}$$

The equations use these variables.

Tbrake	Brake torque
F	Fuel mass per injection
Fcmd, Fmax	Commanded and maximum fuel mass per injection, respectively
Ttarget, Tcmd, Tmax	Target, commanded, and maximum torque, respectively
τbst	Boost time constant
τbst,rising, τbst,falling	Boost rising and falling time constant, respectively
τeng	Final time constant
τnat	Time constant below the boost torque speed line
ƒbst(N)	Boost torque/speed line
N	Engine speed

Dependencies

Selecting Include turbocharger lag effect enables these parameters:

• Boost torque line, f_tbrake_bst

• Time constant below boost line, tau_nat

• Rising maximum fuel mass boost time constant, tau_bst_rising

• Falling maximum fuel mass boost time constant, tau_bst_falling

Input engine temperature — Create input port

off (default) | on

Select this to create the EngTemp input port.

The lookup tables, developed with the Model-Based Calibration Toolbox, are functions of injected fuel mass, F, engine torque, T, engine speed, N, and engine temperature, Temp_Eng.

Input Command Setting	Input Engine Temperature Parameter Setting	Lookup Tables
Fuel mass	off	ƒ(F,N)
	on	ƒ(F,N,TempEng)
Torque	off	ƒ(T,N)
	on	ƒ(T,N,TempEng)

Configuration

Calibrate Maps — Calibrate tables with measured data

selection

If you have Model-Based Calibration Toolbox, click Calibrate Maps to virtually calibrate the 2D lookup tables using measured data. The dialog box steps through these tasks.

Task	Description
Import firing data	Import this loss data from a file. For example, open <matlabroot>/toolbox/mbc/mbctraining/CiEngineData.xlsx. For more information, see Using Data (Model-Based Calibration Toolbox). Input command Required Data Optional Data Fuel mass Engine speed, rpm Commanded fuel mass per injection, mg Engine torque, N·m Air mass flow rate, kg/s Brake specific fuel consumption, g/(kW·h) CO2 mass flow rate, kg/s CO mass flow rate, kg/s Exhaust temperature, K Fuel mass flow rate, kg/s HC mass flow rate, kg/s NOx mass flow rate, kg/s Particulate matter mass flow rate, kg/s Torque Engine speed, rpm Engine torque, N·m Collect firing data at steady-state operating conditions when injectors deliver the fuel. Data should cover the engine speed and torque operating range. Model-Based Calibration Toolbox uses the firing data boundary as the maximum torque. To filter or edit the data, select Edit in Application. The Model-Based Calibration Toolbox Data Editor opens.
Import non-firing data	Import this non-firing data from a file. For example, open <matlabroot>/toolbox/mbc/mbctraining/CiEngineData.xlsx. Engine speed, rpm Engine torque, N·m Collect non-firing (motoring) data at steady-state operating conditions when fuel is cut off. All non-firing torque points must be less than zero. Non-firing data is a function of engine speed only.
Generate response models	For both firing and non-firing data, the Model-Based Calibration Toolbox uses test plans to fit data to Gaussian process models (GPMs). To assess or adjust the response model fit, select Edit in Application. The Model-Based Calibration Toolbox Model Browser opens. For more information, see Model Assessment (Model-Based Calibration Toolbox).
Generate calibration	Model-Based Calibration Toolbox calibrates the firing and non-firing response models and generates calibrated tables. To assess or adjust the calibration, select Edit in Application. The Model-Based Calibration Toolbox CAGE Browser opens. For more information, see Calibration Lookup Tables (Model-Based Calibration Toolbox).
Update block parameters	Update the block lookup table and breakpoint parameters with the calibration.

Dependencies

To enable this parameter, clear Input engine temperature.

Breakpoints for commanded fuel mass input, f_tbrake_f_bpt — Breakpoints

1-by-M vector

Breakpoints, in mg/inj.

Dependencies

Setting Input command to Fuel mass enables this parameter.

Breakpoints for commanded torque input, f_tbrake_t_bpt — Breakpoints

1-by-M vector

Breakpoints, in N·m.

Dependencies

Setting Input command to Torque enables this parameter.

Breakpoints for engine speed input, f_tbrake_n_bpt — Breakpoints

1-by-N vector

Breakpoints, in rpm.

Breakpoints for temperature input, f_tbrake_engtmp_bpt — Breakpoints

[233.15 273.15 373.15] (default) | 1-by-L vector

Breakpoints, in K.

Dependencies

To enable this parameter, select Input engine temperature.

Number of cylinders, NCyl — Number

4 (default) | scalar

Number of cylinders.

Crank revolutions per power stroke, Cps — Crank revolutions

2 (default) | scalar

Crank revolutions per power stroke.

Total displaced volume, Vd — Volume

0.0015 (default) | scalar

Volume displaced by engine, in m^3.

Fuel lower heating value, Lhv — Heating value

45e6 (default) | scalar

Fuel lower heating value, LHV, in J/kg.

Fuel specific gravity, Sg — Specific gravity

0.832 (default) | scalar

Specific gravity of fuel, Sg_fuel, dimensionless.

Ideal gas constant air, Rair — Constant

287 (default) | scalar

Ideal gas constant of air and residual gas entering the engine intake port, in J/(kg·K).

Air standard pressure, Pstd — Pressure

101325 (default) | scalar

Standard air pressure, in Pa.

Air standard temperature, Tstd — Temperature

293.15 (default) | scalar

Standard air temperature, in K.

Boost torque line, f_tbrake_bst — Boost lag

[90,95,95,95,96,100,104,104,104,100,95,85,75,67,60,55] (default) | 1-by-M vector

Boost torque line, ƒ_bst(N), in N·m.

Dependencies

To enable this parameter, select Include turbocharger lag effect.

Time constant below boost line — Time constant below

0.1 (default) | scalar

Time constant below boost line, τ_nat, in s.

Dependencies

To enable this parameter, select Include turbocharger lag effect.

Rising maximum fuel mass boost time constant, tau_bst_rising — Rising time constant

1.0 (default) | scalar

Rising maximum fuel mass boost time constant, τ_bst,rising, in s.

Dependencies

To enable this parameter, select Include turbocharger lag effect.

Falling maximum fuel mass boost time constant, tau_bst_falling — Falling time constant

0.7 (default) | scalar

Falling maximum fuel mass boost time constant, τ_bst,falling, in s.

Dependencies

To enable this parameter, select Include turbocharger lag effect.

Turbocharger time constant blend fuel mass fraction, f_blend_frac — Time constant

0.01 (default) | scalar

Turbocharger time constant blend fuel mass fraction, in s.

Dependencies

To enable this parameter, select Include turbocharger lag effect.

Power

Brake torque map, f_tbrake — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine brake torque lookup table is a function of commanded fuel mass and engine speed, $T_{brake}$ = ƒ(F, N), where: $T_{brake}$ is engine torque, in N·m. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine brake torque lookup table is a function of target torque and engine speed, $T_{brake}$ = ƒ(Ttarget, N), where: $T_{brake}$ is engine torque, in N·m. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot brake torque map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

Brake torque map, f_tbrake_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine brake torque lookup table is a function of commanded fuel mass and engine speed, $T_{brake}$ = ƒ(F, N, TempEng), where: $T_{brake}$ is engine torque, in N·m. F is commanded fuel mass, in mg per injection. TempEng is engine temperature, in K.
Torque	The engine brake torque lookup table is a function of target torque and engine speed, $T_{brake}$ = ƒ(Ttarget, N, TempEng), where: $T_{brake}$ is engine torque, in N·m. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

Air

Air mass flow map, f_air — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The air mass flow lookup table is a function of commanded fuel mass and engine speed, ${\dot{m}}_{intk}$ = ƒ(Fmax, N), where: ${\dot{m}}_{intk}$ is engine air mass flow, in kg/s. Fmax is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The air mass flow lookup table is a function of maximum torque and engine speed, ${\dot{m}}_{intk}$ = ƒ(Tmax, N), where: ${\dot{m}}_{intk}$ is engine air mass flow, in kg/s. Tmax is maximum torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot air mass map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

Air mass flow map, f_air_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The air mass flow lookup table is a function of commanded fuel mass and engine speed, ${\dot{m}}_{intk}$ = ƒ(Fmax, N, TempEng), where: ${\dot{m}}_{intk}$ is engine air mass flow, in kg/s. Fmax is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The air mass flow lookup table is a function of maximum torque and engine speed, ${\dot{m}}_{intk}$ = ƒ(Tmax, N, TempEng), where: ${\dot{m}}_{intk}$ is engine air mass flow, in kg/s. Tmax is maximum torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

Fuel

Fuel flow map, f_fuel — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine fuel flow lookup table is a function of commanded fuel mass and engine speed, MassFlow= ƒ(F, N), where: MassFlow is engine fuel mass flow, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine fuel flow lookup table is a function of target torque and engine speed, MassFlow = ƒ(Ttarget, N), where: MassFlow is engine fuel mass flow, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot fuel flow map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

Fuel flow map, f_fuel_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine fuel flow lookup table is a function of commanded fuel mass, engine speed, and engine temperature, MassFlow= ƒ(F, N, TempEng), where: MassFlow is engine fuel mass flow, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The engine fuel flow lookup table is a function of target torque and engine speed, and engine temperature, MassFlow = ƒ(Ttarget, N, TempEng), where: MassFlow is engine fuel mass flow, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

Temperature

Exhaust temperature map, f_texh — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine exhaust temperature table is a function of commanded fuel mass and engine speed, Texh= ƒ(F, N), where: Texhis exhaust temperature, in K. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine exhaust temperature table is a function of target torque and engine speed, Texh = ƒ(Ttarget, N), where: Texh is exhaust temperature, in K. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot exhaust temperature map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

Exhaust temperature map, f_texh_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine exhaust temperature table is a function of commanded fuel mass and engine speed, Texh= ƒ(F, N, TempEng), where: Texhis exhaust temperature, in K. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The engine exhaust temperature table is a function of target torque and engine speed, Texh = ƒ(Ttarget, N, TempEng), where: Texh is exhaust temperature, in K. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

Efficiency

BSFC map, f_eff — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The brake-specific fuel consumption (BSFC) efficiency is a function of commanded fuel mass and engine speed, BSFC= ƒ(F, N), where: BSFC is BSFC, in g/kWh. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The brake-specific fuel consumption (BSFC) efficiency is a function of target torque and engine speed, BSFC = ƒ(Ttarget, N), where: BSFC is BSFC, in g/kWh. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot BSFC map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

BSFC map, f_eff_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The brake-specific fuel consumption (BSFC) efficiency is a function of commanded fuel mass and engine speed, BSFC= ƒ(F, N, TempEng), where: BSFC is BSFC, in g/kWh. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The brake-specific fuel consumption (BSFC) efficiency is a function of target torque and engine speed, BSFC = ƒ(Ttarget, N, TempEng), where: BSFC is BSFC, in g/kWh. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

HC

EO HC map, f_hc — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine-out hydrocarbon emissions are a function of commanded fuel mass and engine speed, EO HC= ƒ(F, N), where: EO HC is engine-out hydrocarbon emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine-out hydrocarbon emissions are a function of target torque and engine speed, EO HC = ƒ(Ttarget, N), where: EO HC is engine-out hydrocarbon emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot EO HC map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

EO HC map, f_hc_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine-out hydrocarbon emissions are a function of commanded fuel mass and engine speed, EO HC= ƒ(F, N, TempEng), where: EO HC is engine-out hydrocarbon emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The engine-out hydrocarbon emissions are a function of target torque and engine speed, EO HC = ƒ(Ttarget, N, TempEng), where: EO HC is engine-out hydrocarbon emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

CO

EO CO map, f_co — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine-out carbon monoxide emissions are a function of commanded fuel mass and engine speed, EO CO= ƒ(F, N), where: EO CO is engine-out carbon monoxide emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine-out carbon monoxide emissions are a function of target torque and engine speed, EO CO = ƒ(Ttarget, N), where: EO CO is engine-out carbon monoxide emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot EO CO map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

EO CO map, f_co_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine-out carbon monoxide emissions are a function of commanded fuel mass and engine speed, EO CO= ƒ(F, N, TempEng), where: EO CO is engine-out carbon monoxide emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The engine-out carbon monoxide emissions are a function of target torque and engine speed, EO CO = ƒ(Ttarget, N, TempEng), where: EO CO is engine-out carbon monoxide emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

NOx

EO NOx map, f_nox — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine-out nitric oxide and nitrogen dioxide emissions are a function of commanded fuel mass and engine speed, EO NOx= ƒ(F, N), where: EO NOx is engine-out nitric oxide and nitrogen dioxide emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine-out nitric oxide and nitrogen dioxide emissions are a function of target torque and engine speed, EO NOx = ƒ(Ttarget, N), where: EO NOx is engine-out nitric oxide and nitrogen dioxide emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot EO NOx map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

EO NOx map, f_nox_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine-out nitric oxide and nitrogen dioxide emissions are a function of commanded fuel mass, engine speed, and engine temperature, EO NOx= ƒ(F, N, TempEng), where: EO NOx is engine-out nitric oxide and nitrogen dioxide emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The engine-out nitric oxide and nitrogen dioxide emissions are a function of target torque, engine speed, and engine temperature, EO NOx = ƒ(Ttarget, N, TempEng), where: EO NOx is engine-out nitric oxide and nitrogen dioxide emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

CO2

EO CO2 map, f_co2 — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine-out carbon dioxide emissions are a function of commanded fuel mass and engine speed, EO CO2= ƒ(F, N), where: EO CO2 is engine-out carbon dioxide emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine-out carbon dioxide emissions are a function of target torque and engine speed, EO CO2 = ƒ(Ttarget, N), where: EO CO2 is engine-out carbon dioxide emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot CO2 map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

EO CO2 map, f_co2_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine-out carbon dioxide emissions are a function of commanded fuel mass, engine speed, and engine temperature, EO CO2= ƒ(F, N, TempEng), where: EO CO2 is engine-out carbon dioxide emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The engine-out carbon dioxide emissions are a function of target torque, engine speed, and engine temperature, EO CO2 = ƒ(Ttarget, N, TempEng), where: EO CO2 is engine-out carbon dioxide emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

PM

EO PM map, f_pm — 2D lookup table

M-by-N matrix

Input Command Setting	Description
Fuel mass	The engine-out PM emissions are a function of commanded fuel mass and engine speed, where: EO PM is engine-out PM emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm.
Torque	The engine-out PM emissions are a function of target torque and engine speed, EO PM = ƒ(Ttarget, N), where: EO PM is engine-out PM emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm.

Dependencies

To enable this parameter, clear Input engine temperature.

Plot EO PM map — Plot table

button

Click to plot table.

Dependencies

To enable this parameter, clear Input engine temperature.

EO PM map, f_pm_3d — 3D lookup table

M-by-N-by-L array

Input Command Setting	Description
Fuel mass	The engine-out PM emissions are a function of commanded fuel mass, engine speed, and engine temperature, where: EO PM is engine-out PM emissions, in kg/s. F is commanded fuel mass, in mg per injection. N is engine speed, in rpm. TempEng is engine temperature, in K.
Torque	The engine-out PM emissions are a function of target torque, engine speed, and engine temperature, EO PM = ƒ(Ttarget, N, T), where: EO PM is engine-out PM emissions, in kg/s. Ttarget is target torque, in N·m. N is engine speed, in rpm. TempEng is engine temperature, in K.

Dependencies

To enable this parameter, select Input engine temperature.

Extended Capabilities

C/C++ Code Generation
Generate C and C++ code using Simulink® Coder™.

Version History

Introduced in R2017a