Flatness-based hypersonic reentry guidance of a lifting-body vehicle

Control Engineering Practice

Volumn 17, Issue 5, 2009, Pages 588-596

  Morio, Vincent ^a   Cazaurang, Franck ^a   Vernis, Philippe ^b  

^a UNIVERSITÉ DE BORDEAUX   (France)

^b AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

Flatness theory; Hypersonic reentry guidance; Monte Carlo simulations; Nonlinear dynamic inversion

Indexed keywords

AUTOMOBILE BODIES; MONTE CARLO METHODS; OPTICAL RESOLVING POWER; PROPORTIONAL CONTROL SYSTEMS; THREE TERM CONTROL SYSTEMS;

ANGLE-OF-ATTACK; AZIMUTH ERRORS; CLOSED LOOPS; COMPUTATIONAL RESOURCES; DEGREE OF FREEDOMS; DESIGN PARAMETERS; FLATNESS THEORY; GUIDANCE ALGORITHMS; GUIDANCE COMMANDS; GUIDANCE LAWS; GUIDANCE STRATEGIES; HYPERSONIC REENTRY GUIDANCE; LINE DESIGNS; MONTE CARLO; MONTE CARLO SIMULATIONS; NONLINEAR DYNAMIC INVERSION; PID CONTROLLERS; SELF-ADAPTIVE; VEHICLE PARAMETERS;

REENTRY;

EID: 63149158550     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.conengprac.2008.10.018     Document Type: Article

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