Robust adaptive sliding mode attitude maneuvering and vibration damping of three-axis-stabilized flexible spacecraft with actuator saturation limits

Nonlinear Dynamics

Volumn 55, Issue 4, 2009, Pages 301-321

  Hu, Qinglei ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Adaptive sliding mode control; Attitude maneuver; Flexible spacecraft; Saturation input; Vibration control

Indexed keywords

ACTUATORS; CONTROL SYSTEMS; CONTROL THEORY; CONTROLLERS; FEEDBACK; POLARIZATION; ROBUST CONTROL; SLIDING MODE CONTROL; SPACECRAFT; VIBRATION CONTROL;

ACTIVE VIBRATION SUPPRESSIONS; ACTUATOR SATURATIONS; ADAPTIVE CONTROLLERS; ADAPTIVE SLIDING MODE CONTROL; ADAPTIVE SLIDING MODE CONTROLLERS; ATTITUDE CONTROL SYSTEMS; ATTITUDE MANEUVER; BOUNDED PARAMETERS; CONTROL INPUTS; DUAL STAGES; EXPONENTIAL CONVERGENCES; FLEXIBLE SPACECRAFT; INDUCED VIBRATIONS; LINEAR-QUADRATIC REGULATORS; LYAPUNOV ANALYSIS; MANEUVERING CONTROLS; NUMERICAL SIMULATIONS; POSITIVE POSITION FEEDBACKS; ROBUST ADAPTIVE; SATURATION INPUT; SMART MATERIALS; STEPPING STONES; THREE-AXIS; UNIFORM ULTIMATE BOUNDEDNESS; UPPER BOUNDS; VIBRATION SUPPRESSIONS; VIBRATION-DAMPING;

ADAPTIVE CONTROL SYSTEMS;

EID: 59349118241     PISSN: 0924090X     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11071-008-9363-1     Document Type: Article

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