Direct fault tolerant RLV attitude control - A singular perturbation approach

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Zhu, J J ^a   Lawrence, D A ^a   Fisher, J ^a   Shtessel, Y B ^b   Hodel, A S ^c   Lu, P ^d  

^a OHIO UNIVERSITY   (United States)

^b UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

^c AUBURN UNIVERSITY   (United States)

^d IOWA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ATTITUDE CONTROL; BANDWIDTH; DISPERSIONS; EIGENVALUES AND EIGENFUNCTIONS; FAULT TOLERANCE; LAUNCH VEHICLES; PERTURBATION TECHNIQUES; REUSABILITY; REUSABLE ROCKETS;

FAULT TOLERANT CONTROL; MULTI-INPUT , MULTI-OUTPUT SYSTEMS; RE-USABLE LAUNCH VEHICLES (RLV); RECEDING HORIZON OPTIMAL CONTROL; REUSABLE LAUNCH VEHICLES; SINGULAR PERTURBATION APPROACHES; SINGULAR PERTURBATION THEORY; SINGULAR PERTURBATIONS;

FEEDBACK;

EID: 85086488922     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4778     Document Type: Conference Paper

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