WOLFRAM SYSTEM MODELER

ControlLogic

Satellite controller

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.

 

Connectors (4)

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

target_height

Type: Constant

vectorAdd2

Type: VectorAdd

forward_controller

Type: LimPID

target_force

Type: Constant

gain1

Type: Gain

altitudeConverter2

Type: ForceConversion

launchSwitch

Type: BooleanStep

Used in Examples (1)

SatelliteScenario

EducationExamples.AerospaceEngineering.Satellite

Model scenario of the launch and flight of a satellite.