Spacecraft Rigid Body Dynamics (attitude) library block (Scripts) Publisher's description
from Paul Acquatella
The dynamics of the rotational motion of a rigid body is simulated with this functional library block
The dynamics of the rotational motion of a rigid body is simulated with this functional library block. This block is intended for simulation (academic) purposes, where the time history of the angular velocity vector is provided.
This library block is part of a library currently being developed for the simulation of spacecraft attitude control systems.
System Requirements:MATLAB 7.11 (2010b)
Program Release Status: New Release
Program Install Support: Install and Uninstall