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WOLFRAM SYSTEM MODELER

SatelliteMass

Models the mass of the satellite

Diagram

In[1]:=

SystemModel["EducationExamples.AerospaceEngineering.Satellite.Components.SatelliteMass"]

Out[1]:=

This component models the mass of the satellite.

	frame_a	Type: Frame_a Description: Coordinate system fixed to the component with one cut-force and cut-torque (filled rectangular icon)

frame_a

Description: Coordinate system fixed to the component with one cut-force and cut-torque (filled rectangular icon)

	satellite	Type: Body Description: Rigid body with mass, inertia tensor and one frame connector (12 potential states)

satellite

Type: Body

Description: Rigid body with mass, inertia tensor and one frame connector (12 potential states)

EducationExamples.AerospaceEngineering.Satellite

Model scenario of the launch and flight of a satellite.