WOLFRAM SYSTEM MODELER

SatelliteScenario

Model scenario of the launch and flight of a satellite.

Diagram

Wolfram Language

In[1]:=
SystemModel["IndustryExamples.AerospaceDefense.Satellite.SatelliteScenario"]
Out[1]:=

Information

Model a satellite with a combination of 3D mechanics and block-based control logic. The satellite is launched from the Earth's surface with a launch sequence. Then a control logic subsystem adjusts altitude and velocity via thrusters. The Wolfram Language is used to design the parameters of the control system.

Design Controller

Compare different controller options by the altitude and energy expenditure.

Visualize Trajectory

Visualize the satellite using Wolfram Language functionality for 3D graphics. The images show the satellite path with and without controller.

In order to get the full experience of this example, you need a desktop Wolfram Language product. A free trial download is available at www.wolfram.com/mathematica/trial/

For the full example, open the accompanying notebook Satellite.nb.

Parameters (7)

launchVehicleMass

Value: 450000

Type: Mass (kg)

Description: Mass of rigid body

altitudeController_k

Value: 10

Type: Real

Description: Gain of controller

altitudeController_Td

Value: 2000

Type: Time (s)

Description: Time constant of Derivative block

forwardController_k

Value: 0.1

Type: Real

Description: Gain of controller

forwardController_Td

Value: 1000

Type: Time (s)

Description: Time constant of Derivative block

forwardController_yMax

Value: 1000000

Type: Real

Description: Upper limit of output

altitudeController_yMax

Value: 1000000

Type: Real

Description: Upper limit of output

Components (9)

world

Type: World

Description: World coordinate system + gravity field + default animation definition

force

Type: WorldForce

Description: External force acting at frame_b, defined by 3 input signals and resolved in frame world, frame_b or frame_resolve

distance

Type: Distance

Description: Measure the distance between the origins of two frame connectors

satellite_position_absolute

Type: AbsolutePosition

Description: Measure absolute position vector of the origin of a frame connector

satellite_position_over_earth

Type: AbsolutePosition

Description: Measure absolute position vector of the origin of a frame connector

earth

Type: Earth

Description: Models the mass of the earth

controlLogic

Type: ControlLogic

Description: Satellite controller

satellite

Type: SatelliteMass

Description: Models the mass of the satellite

satellite_velocity

Type: AbsoluteVelocity

Description: Measure absolute velocity vector of origin of frame connector