WOLFRAM SYSTEM MODELER

Rocket

Body and shape for rocket

Diagram

Wolfram Language

In[1]:=
SystemModel["DocumentationExamples.Control.VectoredThrustAircraft.Rocket"]
Out[1]:=

Information

Wolfram Language Documentation Examples

This library contains models used in the documentation of system modeling functionality in Wolfram Language. These examples and this library can be explored in the Wolfram Language documentation.

Parameters (3)

bodyVolume

Value: 4165.934 * uniformSizeScale ^ 3

Type: Volume (m³)

Description: Volume of the body
uniformDensity

Value: 7700

Type: Density (kg/m³)

Description: Uniform density of the body. If it is not provided, it defaults to 7.7 g.cm-3
uniformSizeScale

Value: 1

Type: Length (m)

Description: Uniform size scaling: length in meters of a unit of length of original region

Connectors (1)

frame_a

Type: Frame_a

Description: Coordinate system fixed to the component with one cut-force and cut-torque

Components (3)

world

Type: World

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

Type: Body

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

Type: FixedShape

Description: Visualizing an elementary shape with dynamically varying shape attributes (has one frame connector)

Used in Examples (1)

VectoredThrustAircraft

DocumentationExamples.Control

Simplified model of a rockect with vectored thrust