On the design of a flatness-based guidance algorithm for the terminal area energy management of a winged-body vehicle

IFAC Proceedings Volumes (IFAC-PapersOnline)

Volumn 17, Issue PART 1, 2007, Pages 563-568

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

^a UNIVERSITÉ BORDEAUX 1   (France)

^b AIRBUS DEFENCE AND SPACE   (Germany)

Author keywords

Differential flatness; Monte carlo simulations; Nonlinear dynamic inversion; Reusable launch vehicle; Taem guidance

Indexed keywords

AIR NAVIGATION; AUTOMATION; ENERGY MANAGEMENT; FLIGHT ENVELOPES; LAUNCH VEHICLES; REUSABILITY; REUSABLE ROCKETS;

DIFFERENTIAL FLATNESS; FLATNESS APPROACHES; FLATNESS THEORIES; GUIDANCE ALGORITHM; GUIDANCE STRATEGY; NONLINEAR DYNAMIC INVERSION; REUSABLE LAUNCH VEHICLES; TERMINAL AREA ENERGY MANAGEMENT;

MONTE CARLO METHODS;

EID: 79960990688     PISSN: 14746670     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.3182/20070625-5-fr-2916.00096     Document Type: Conference Paper

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