WOLFRAM SYSTEM MODELER
EnergyStorageBaseInterface for EnergyStorage model |
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Wolfram Language
In[1]:=
SystemModel["Aircraft.Physical.FixedWing.Parts.Propulsions.EnergyStorages.Interfaces.EnergyStorageBase"]
Out[1]:=
Information
This class is the energy storage base model, which the TankSystem and BatterySystem models extend, and contains the input port for fuel or energy consumption and the aircraft reference point frame.
In this class, the parameters and variables that are used in both energy system models are declared. Additionally, the calculation for the first time derivative of the energy that is left in the energy storage, i.e input power to the propulsion system, is performed in this model.
Parameters (3)
| weightEst |
Value: Type: Boolean Description: true, if weight estimation method is used for masses, center of mass location and inertia tensor |
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| wFus |
Value: Type: Length (m) Description: Fuselage maximum width |
| engineType |
Value: Type: Integer Description: Type of engine (0 = piston, 1 = turboprop, 2 = turbojet, 3 = turbofan, 4 = electric) |
Outputs (1)
| xEf |
Type: Real Description: State of energy storage energy |
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Connectors (2)
Extended by (3)
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Aircraft.Physical.FixedWing.Parts.Propulsions.Interfaces.ConventionalPropulsion Type of energy storage used in the propulsion system |
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Aircraft.Physical.FixedWing.Parts.Propulsions.EnergyStorages Model for battery system |
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Aircraft.Physical.FixedWing.Parts.Propulsions.EnergyStorages Model for fuel tank system |