Output feedback back-stepping control for a generic Hypersonic Vehicle via small-gain theorem

Aerospace Science and Technology

Volumn 23, Issue 1, 2012, Pages 409-417

  Zong, Qun ^a   Ji, Yuehui ^a   Zeng, Fanlin ^a   Liu, Helong ^a  

^a TIANJIN UNIVERSITY   (China)

Author keywords

Back stepping technique; Hypersonic Vehicle; Output feedback control; Small gain theorem

Indexed keywords

CONTROL SCHEMES; DYNAMIC OUTPUT-FEEDBACK; GENERIC HYPERSONIC VEHICLES; LONGITUDINAL DYNAMICS; MULTI VARIABLES; NON-LINEAR CONTROLLERS; NON-LINEAR MODEL; NON-LINEAR OBSERVER; OUTPUT FEEDBACK; OUTPUT FEEDBACK CONTROLS; REFERENCE TRAJECTORIES; SMALL GAIN THEOREM; STABILITY ANALYSIS; SYSTEM OUTPUT; VEHICLE MODEL;

COMPUTER SIMULATION; FEEDBACK CONTROL; HYPERSONIC VEHICLES;

HYPERSONIC AERODYNAMICS;

EID: 84869502242     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2011.09.012     Document Type: Conference Paper

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