WOLFRAM SYSTEM MODELER

Blocks

Blocks to be used to model the aircraft motion in linearized state space representation

Package Contents

LongitudinalDerivatives

Calculates longitudinal stability and control derivatives

LateralDerivatives

Calculates lateral stability and control derivatives

LongitudinalMotion

State space representation of longitudinal motion

LateralMotion

State space representation of lateral motion

PositionAndOrientation

Calculates the position, orientation and velocities of the aircraft in the world frame

Body2Fixed

Transformation of linear and angular velocity from body frame to world frame

TrimCalculator

Calculates trimmed conditions for given flight conditions

Information

This package contains the components that are required to build complete aircraft models.

Wolfram Language

In[1]:=
SystemModel["Aircraft.StateSpace.FixedWing.Blocks"]
Out[1]:=