Fault-tolerant optimal trajectory generation for reusable launch vehicles

Journal of Guidance, Control, and Dynamics

Volumn 30, Issue 6, 2007, Pages 1794-1802

  Shaffer, Patrick J ^a,c   Ross, I Michael ^a,d,e   Oppenheimer, Michael W ^b,e,f   Doman, David B ^b,e,f   Bollino, Kevin P ^a,g  

^a NAVAL POSTGRADUATE SCHOOL   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c Space and Naval Warfare Systems Center Pacific   (United States)

^d Department of Mechanical and Astronautical Engineering ^*  (United States)

^e AIAA   (United States)

^f Building 146   (United States)

^g USAF   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DEGREES OF FREEDOM (MECHANICS); DRAG; FAULT TOLERANCE; MATHEMATICAL MODELS; PERTURBATION TECHNIQUES; TRAJECTORIES;

AERODYNAMIC FORCES; INNER-LOOP CONTROL LAWS; REUSABLE LAUNCH VEHICLES; TRAJECTORY OPTIMIZATION;

REUSABLE ROCKETS;

EID: 36849068951     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.27699     Document Type: Article

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