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