Comparison of two linearization methods for optimal attitude maneuver of a non-linear flexible spacecraft

IMA Journal of Mathematical Control and Information

Volumn 23, Issue 2, 2006, Pages 127-136

  Zheng, Jianhua ^a  

^a CENTER FOR SPACE SCIENCE AND APPLIED RESEARCH   (China)

Author keywords

Non linear flexible spacecraft; Optimal attitude maneuver; Recursive approximating sequence approach linearization method; Small sphere approximating approach linearization method; Vibration suppression control

Indexed keywords

COMPUTER SIMULATION; LINEARIZATION; MANEUVERABILITY; SPACECRAFT; TIME VARYING CONTROL SYSTEMS; VIBRATION CONTROL;

NON-LINEAR FLEXIBLE SPACECRAFT; OPTIMAL ATTITUDE MANEUVER; RECURSIVE APPROXIMATING SEQUENCE APPROACH LINEARIZATION METHOD; SMALL SPHERE APPROXIMATING APPROACH LINEARIZATION METHOD; VIBRATION SUPPRESSION CONTROL;

NONLINEAR CONTROL SYSTEMS;

EID: 33644881089     PISSN: 02650754     EISSN: 14716887     Source Type: Journal    
DOI: 10.1093/imamci/dni048     Document Type: Article

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