Quaternion feedback for spacecraft large angle maneuvers

Journal of Guidance, Control, and Dynamics

Volumn 8, Issue 3, 1985, Pages 360-365

  Wie, Bong ^a,b   Barb, Peter M ^a,b  

^a Ford Aerospace Communications Corporation ^*  (United States)

^b Systems Analysis Department ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; SYSTEM STABILITY - LYAPUNOV METHODS;

QUATERNION FEEDBACK; REORIENTATION MANEUVERS;

SPACECRAFT;

EID: 0022066858     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.19988     Document Type: Article

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