WOLFRAM SYSTEM MODELER
ControlLogicSatellite controller |
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SystemModel["EducationExamples.AerospaceEngineering.Satellite.Components.ControlLogic"]

| height |
Type: RealInput Description: 'input Real' as connector |
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|---|---|---|
| y |
Type: RealOutput[3] Description: 'output Real' as connector |
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| position |
Type: RealInput[3] Description: 'input Real' as connector |
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| direction |
Type: RealInput[3] Description: 'input Real' as connector |
| vectorAdd1 |
Type: VectorAdd Description: Adds threedimensional vectors |
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|---|---|---|
| altitudeConverter1 |
Type: ForceConversion Description: Models the propulsion force |
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| satelliteLaunchControl1 |
Type: LaunchControl Description: Models launch forces on the satellite |
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| controller |
Type: LimPID Description: P, PI, PD, and PID controller with limited output, anti-windup compensation, setpoint weighting and optional feed-forward |
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| target_height |
Type: Constant Description: Generate constant signal of type Real |
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| vectorAdd2 |
Type: VectorAdd Description: Adds threedimensional vectors |
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| forward_controller |
Type: LimPID Description: P, PI, PD, and PID controller with limited output, anti-windup compensation, setpoint weighting and optional feed-forward |
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| target_force |
Type: Constant Description: Generate constant signal of type Real |
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| gain1 |
Type: Gain Description: Output the product of a gain value with the input signal |
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| altitudeConverter2 |
Type: ForceConversion Description: Models the propulsion force |
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| launchSwitch |
Type: BooleanStep Description: Generate step signal of type Boolean |
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EducationExamples.AerospaceEngineering.Satellite Model scenario of the launch and flight of a satellite. |