Spacecraft Attitude Kinematics in terms of Rodrigues Parameters library block (Scripts) Publisher's description
from Paul Acquatella
The attitude kinematics of a rigid body is simulated with this functional library block.
The attitude kinematics 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 attitude in term of Rodrigues Parameters is provided. See  for reference on the subject.
This library block is part of a library currently being developed for the simulation of spacecraft attitude control systems.
 Tsiotras, P., "Stabilization and Optimality Results for the Attitude Control Problem," AIAA Journal of Guidance, Control, and Dynamics, Vol. 19, No. 4, pp. 772-779, 1996.
System Requirements:MATLAB 7.11 (2010b)
Program Release Status: New Release
Program Install Support: Install and Uninstall