Investigation of active vibration suppression of a flexible satellite using magnetic attitude control

AIAA Guidance, Navigation, and Control Conference 2011

Volumn , Issue , 2011, Pages

  Findlay, Everett J ^a   Forbes, James R ^b   Liu, Hugh H T ^a   de Ruiter, Anton ^c   Damaren, Christopher J ^a   Lee, James ^d  

^a UNIVERSITY OF TORONTO   (Canada)

^b MCGILL UNIVERSITY   (Canada)

^c CARLETON UNIVERSITY   (Canada)

^d CANADIAN SPACE AGENCY   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE CONTROL; CONTROL RODS; FLEXIBLE STRUCTURES; SATELLITES;

ACTIVE VIBRATION SUPPRESSION; FLEXIBLE SATELLITES; INITIAL CONDITIONS; MAGNETIC ATTITUDE CONTROLS; MAGNETIC TORQUE RODS; MOMENTUM BIASED SATELLITE; REACTION WHEELS; TIME INVARIANTS;

CONTROLLERS;

EID: 85087535669     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2011-6706     Document Type: Conference Paper

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