WOLFRAM SYSTEM MODELER
ControlLogicSatellite controller |
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Diagram
Wolfram Language
In[1]:=
SystemModel["EducationExamples.AerospaceEngineering.Satellite.Components.ControlLogic"]
Out[1]:=
Information
Control Logic
Description
This component models the control logic of a satellite. It contains two controllers and some supporting structure around them. The controller components are controller and forward_controller, which control the propulsion forces in the upward and forward directions, respectively. The result of these controllers gets added to the launch sequence forces from the launch component.
View the model diagram for this model.
Terms and Conditions of Use
Terms and Conditions of UseConnectors (4)
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height |
Type: RealInput |
|---|---|---|
 |
y |
Type: RealOutput[3] |
|
position |
Type: RealInput[3] |
|
direction |
Type: RealInput[3] |
Components (11)
 |
vectorAdd1 |
Type: VectorAdd |
|---|---|---|
 |
altitudeConverter1 |
Type: ForceConversion |
 |
satelliteLaunchControl1 |
Type: LaunchControl |
 |
controller |
Type: LimPID |
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target_height |
Type: Constant |
|
vectorAdd2 |
Type: VectorAdd |
|
forward_controller |
Type: LimPID |
|
target_force |
Type: Constant |
 |
gain1 |
Type: Gain |
|
altitudeConverter2 |
Type: ForceConversion |
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launchSwitch |
Type: BooleanStep |
Used in Examples (1)
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EducationExamples.AerospaceEngineering.Satellite Model scenario of the launch and flight of a satellite. |