In this paper the spacecraft attitude stability problem with external disturbance are considered. A nonlinear attitude controller introducing disturbance suppression for spacecraft is designed using internal model principle. The effectiveness and robustness are demonstrated through a series of numerical simulations.
Nonlinear Attitude Control for Spacecraft
Applied Mechanics and Materials ; 394 ; 421-426
2013-09-03
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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