Variable structure maneuvering control with time-varying sliding surface and active vibration damping of flexible spacecraft with input saturation

Acta Astronautica

Volumn 64, Issue 11-12, 2009, Pages 1085-1108

  Hu, Qinglei ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

Attitude maneuver; Flexible spacecraft; Input saturation; Variable structure control; Vibration control

Indexed keywords

ATTITUDE CONTROL; CONTROLLERS; DAMPING; DC MOTORS; MACHINE DESIGN; PIEZOELECTRIC ACTUATORS; POLARIZATION; SPACECRAFT; SPATIAL VARIABLES CONTROL; STRAIN RATE; STRUCTURAL DESIGN; SURFACES; TIME VARYING SYSTEMS; VARIABLE STRUCTURE CONTROL; VIBRATION CONTROL; VIBRATORS;

ACTIVE VIBRATION DAMPING; ATTITUDE CONTROL SYSTEMS; ATTITUDE CONTROLLERS; ATTITUDE MANEUVER; CLOSED-LOOP SYSTEMS; CONTROL DESIGN METHODS; CONTROL SATURATIONS; DESIGN APPROACHES; DISCONTINUOUS CONTROLS; DISTURBANCE TORQUES; DUAL STAGES; ELASTIC MODES; ELASTIC VIBRATIONS; FLEXIBLE SPACECRAFT; HYPERBOLIC TANGENT FUNCTIONS; INPUT SATURATION; MANEUVERING CONTROLS; NUMERICAL SIMULATIONS; PARAMETER UNCERTAINTIES; PIEZO-CERAMICS; SENSORS AND ACTUATORS; SHARPNESS FUNCTIONS; SLIDING SURFACES; STRAIN RATE FEEDBACKS; SWITCHING MECHANISMS; THREE-AXIS; TIME-VARYING; USER-DEFINED PARAMETERS; VARIABLE-STRUCTURE CONTROLS; VELOCITY FEEDBACKS; VIBRATION SUPPRESSIONS;

FEEDBACK;

EID: 63549103176     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actaastro.2009.01.009     Document Type: Article

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