WOLFRAM SYSTEM MODELER

VectoredThrustAircraft

Simplified model of a rockect with vectored thrust

Diagram

Wolfram Language

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

uniformSizeScale

Value: 1

Type: Real

Description: Factor by which dimensions of rocket are rescaled

r

Value: 34 * uniformSizeScale

Type: Distance (m)

Description: Distance from point of application of tangential thrust to center of mass

d

Value: 1

Type: TranslationalDampingConstant (N⋅s/m)

Description: Linear air resistance constant

Connectors (5)

fv

Type: RealInput

Description: Vertical thrust in addition to weight compensation, resolved in the rocket frame

ft

Type: RealInput

Description: Tangential thrust acting at distance r from the center of mass, resolved in the rocket frame

fwind

Type: RealInput

Description: Wind force acting on the center of mass of the rocket in the direction of the y-axis, resolved in the laboratory frame

angles

Type: RealOutput[3]

Description: Euler angles from fixed to rocket frame

z

Type: RealOutput

Description: Position of center of mass

Components (11)

world

Type: World

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

fixedTranslation1

Type: FixedTranslation

Description: Fixed translation of frame_b with respect to frame_a

force1

Type: WorldForce

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

force2

Type: WorldForce

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

linearAirResistance

Type: LinearAirResistance

Description: Linear air resistance

add

Type: Add

Description: Output the sum of the two inputs

const

Type: Constant

Description: Generate constant signal of type Real

rocket

Type: Rocket

Description: Body and shape for rocket

fixedTranslation2

Type: FixedTranslation

Description: Fixed translation of frame_b with respect to frame_a

fixedShape1

Type: FixedShape

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

windForce

Type: WorldForce

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