Optimal guidance command generation and tracking for reusable launch vehicle reentry

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006

Volumn 7, Issue , 2006, Pages 4614-4636

  Bollino, Kevin P ^a,c,d   Oppenheimer, Michael W ^b,d,e   Doman, David D ^b,d,e  

^a NAVAL POSTGRADUATE SCHOOL   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c and Control Lab   (United States)

^d AIAA   (United States)

^e Bldg 146 ^*  (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DEGREES OF FREEDOM (MECHANICS); ELECTRONIC GUIDANCE SYSTEMS; LAUNCHING; ROBUSTNESS (CONTROL SYSTEMS); TRACKING (POSITION);

OPTIMAL REFERENCE TRAJECTORIES; PSEUDOSPECTRAL METHOD; VEHICLE REENTRY; WINDUP PREFILTERS;

REENTRY;

EID: 33845760933     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-6691     Document Type: Conference Paper

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