Nonlinear control of a hypersonic vehicle with structural flexibility

Proceedings of the IEEE Conference on Decision and Control

Volumn , Issue , 2008, Pages 578-583

  Fiorentini, Lisa ^a,c   Serrani, Andrea ^a   Bolender, Michael A ^b   Doman, David B ^b  

^a OHIO STATE UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c The Ohio State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALTITUDE CONTROL; ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; STATE FEEDBACK; UNCERTAINTY ANALYSIS;

FIRST PRINCIPLE MODELS; NON-MINIMUM PHASE BEHAVIOR; NONLINEAR ROBUST ADAPTIVE; PARAMETRIC MODELING; REDUCED COMPLEXITY; REFERENCE TRAJECTORIES; STATE FEEDBACK CONTROLLER; STRUCTURAL FLEXIBILITIES;

CONTROLLERS;

EID: 62949143968     PISSN: 07431546     EISSN: 25762370     Source Type: Conference Proceeding    
DOI: 10.1109/CDC.2008.4739001     Document Type: Conference Paper

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