Time-optimal rest-to-rest slewing of multi-mode flexible spacecraft using zvd robustness constraints

1996 Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 1996, Pages 1-9

  Singhose, William E ^a   Pao, Lucy Y ^b   Seering, Warren P ^a  

^a Massachusetts Institute of Technology Cambridge   (United States)

^b University of Colorado at Boulder   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; ERRORS; FLEXIBLE SPACECRAFT; SPACECRAFT;

FINAL STATE; HIGHER MODE; MODEL ERRORS; REACTION JET; RESIDUAL VIBRATIONS; ROBUSTNESS TO MODELING ERRORS; SYSTEM FREQUENCY; TIME-OPTIMAL;

ROBUSTNESS (CONTROL SYSTEMS);

EID: 34047239896     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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