Reusable stellar inertial attitude determination (SIAD) design for spacecraft guidance, navigation & control

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 1, Issue , 2005, Pages 785-789

  Li, Rongsheng ^a   Needelman, David ^a   Fowell, Richard ^a   Tsao, Tung Ching ^a   Wu, Yeong Wei Andy ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FAULT RESPONSE; FLIGHT SOFTWARE; SPACECRAFT ATTITUDE DETERMINATION SENSORS; STELLAR INERTIAL ATTITUDE DETERMINATION (SIAD);

AIRCRAFT; ALGORITHMS; DESIGN; FLIGHT DYNAMICS; KALMAN FILTERING; MISSILES; REENTRY; SENSORS; SPACE APPLICATIONS;

SPACECRAFT;

EID: 29744471000     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (25)

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