Quarternion feedback regulator for spacecraft eigenaxis rotations

Journal of Guidance, Control, and Dynamics

Volumn 12, Issue 3, 1989, Pages 375-380

  Wie, B ^a,b   Weiss, H ^a,b   Arapostathis, A ^a,b  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

^b Department of Aerospace Engineering and Engineering Mechanics ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

MATHEMATICAL TECHNIQUES--EIGENVALUES AND EIGENFUNCTIONS; SYSTEM STABILITY--LYAPUNOV METHODS;

EULER'S EIGENAXIS ROTATION; QUATERNION FEEDBACK REGULATOR; QUATERNION FEEDBACK STABILITY ANALYSIS; SPACECRAFT EIGENAXIS ROTATIONS;

SPACECRAFT;

EID: 0024656129     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.20418     Document Type: Article

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