Adaptive output feedback sliding-mode manoeuvring and vibration control of flexible spacecraft with input saturation

IET Control Theory and Applications

Volumn 2, Issue 6, 2008, Pages 467-478

  Hu, Q ^a  

^a HARBIN INSTITUTE OF TECHNOLOGY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

ARCHITECTURAL DESIGN; COMPUTER NETWORKS; ENGINEERING TECHNOLOGY; FEEDBACK CONTROL; FLEXIBLE STRUCTURES; LATTICE VIBRATIONS; PNEUMATIC CONTROL EQUIPMENT; POWER CONVERTERS; SATURATION (MATERIALS COMPOSITION); SPACECRAFT; TECHNOLOGY; VIBRATIONS (MECHANICAL); VIBRATORS;

(OTDR) TECHNOLOGY; ADAPTIVE OUTPUT FEEDBACK; ATTITUDE CONTROLLER; CONTROL INPUTS; CONTROL LOOPS; CONTROL SCHEMES; CONTROL SYSTEM DESIGNS; FLEXIBLE SPACECRAFT; INPUT SATURATIONS; NUMERICA L RESULTS; PIEZO-CERAMICS; POSITIVE POSITION FEEDBACK (PPF); SENSORS AND ACTUATORS; SLIDING MODE CONTROL (SMC); SLIDING MODES; STABILISATION; STATIC OUTPUT FEEDBACK CONTROL; SYSTEM TRAJECTORIES; UPPER BOUNDS;

ADAPTIVE CONTROL SYSTEMS;

EID: 44649085865     PISSN: 17518644     EISSN: 17518652     Source Type: Journal    
DOI: 10.1049/iet-cta:20070099     Document Type: Article

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