Output stabilization of flexible spacecraft with active vibration suppression

IEEE Transactions on Aerospace and Electronic Systems

Volumn 39, Issue 3, 2003, Pages 747-759

  Di Gennaro, S ^a  

^a UNIVERSITY OF L'AQUILA   (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; CONTROL SYSTEM SYNTHESIS; LYAPUNOV METHODS; MANEUVERABILITY; SYSTEM STABILITY; VIBRATION CONTROL;

FLEXIBLE SPACECRAFT; SPACECRAFT ANGULAR VELOCITY; VIBRATION SUPPRESSION;

SPACECRAFT;

EID: 0344704117     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/TAES.2003.1238733     Document Type: Article

References (23)

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