The large attitude maneuver is studied in this paper. The quarternion form attitude is appilied to avoid the singularity of dynamic equations, and sliding mode control law based on quarternion is desined. The spacecraft attitude dynamics and control model is builted using simulink, which was valided by simulation.
Control and Simulation of Spacecraft's Attitude Control Based on Quaternions
Applied Mechanics and Materials ; 380-384 ; 298-301
2013-08-30
4 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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