Path: Missions/FastReorientation
% Simulate the fast reorientation system and demonstrate quaternion propagation
The routines are: QProp, QIToBDot, and the JPL propagation from the Wong
reference.
-------------------------------------------------------------------------------
References: Wong, E.C. and W.G. Breckenridge, "Inertial Attitude Determination
for a Dual-Spin Planetary Spacecraft", AIAA Journal of Guidance
Navigation, and Control Vol. 6, No. 6, Nov-Dec 1983, pp. 491-8.
-------------------------------------------------------------------------
See also FRSTarg, FRSMPlan, FRSCGen, ShapeFlt, QIToBDot, QMult, QPose,
QTForm, Plot2D, TimeGUI, RK4, Unit, QMultJPL, QProp, RIGModel
-------------------------------------------------------------------------
%
--------------------------------------------------------------------------
Copyright (c) 1997-1998 Princeton Satellite Systems, Inc.
All rights reserved.
--------------------------------------------------------------------------
Since version 2.
--------------------------------------------------------------------------