Geometry and inverse optimality in global attitude stabilization

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 6, 1998, Pages 930-939

  Bharadwaj, S ^a,b   Osipchuk, M ^a   Mease, K D ^a,b   Park, F C ^a,c  

^a University of California at Irvine   (United States)

^b AIAA   (United States)

^c Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTATIONAL GEOMETRY; CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; FUNCTIONS; INVERSE PROBLEMS; LYAPUNOV METHODS; OPTIMAL CONTROL SYSTEMS; SPACECRAFT; SYSTEM STABILITY; TOPOLOGY;

CHEVALLEY'S EXPONENTIAL COORDINATES; GLOBAL ATTITUDE STABILIZATION; LIE GROUPS;

POSITION CONTROL;

EID: 0032207609     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4327     Document Type: Article

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