WOLFRAM SYSTEM MODELER

LaunchControl

Models launch forces on the satellite

Diagram

In[1]:=

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

Out[1]:=

This component models the forces acting on the satellite in a fixed launch sequence.

	y	Type: RealOutput[3] Description: 'output Real' as connector

Description: 'output Real' as connector

	launch_force_z1	Type: Step Description: Generate step signal of type Real
	launch_force_y1	Type: Step Description: Generate step signal of type Real
	launch_force_x1	Type: Step Description: Generate step signal of type Real
	add3	Type: Add Description: Output the sum of the two inputs
	add2	Type: Add Description: Output the sum of the two inputs
	add1	Type: Add Description: Output the sum of the two inputs
	launch_force_z	Type: Step Description: Generate step signal of type Real
	launch_force_y	Type: Step Description: Generate step signal of type Real
	launch_force_x	Type: Step Description: Generate step signal of type Real

EducationExamples.AerospaceEngineering.Satellite.Components

Satellite controller

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