Minimax LQR control design for a hypersonic flight vehicle

16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2009, Pages

  Rehman, Obaid Ur ^a   Fidan, Bariş ^b   Petersen, Ian ^a  

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

^b CSIRO   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ALTITUDE CONTROL; FEEDBACK LINEARIZATION; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; LINEAR CONTROL SYSTEMS; LONGITUDINAL CONTROL; STOCHASTIC SYSTEMS; UNCERTAINTY ANALYSIS; VELOCITY;

ADAPTIVE SLIDING MODE; FEEDBACK LINEARIZATION TECHNIQUE; HYPERSONIC FLIGHT VEHICLES; INTEGRAL QUADRATIC CONSTRAINTS; LINEAR QUADRATIC REGULATOR CONTROL; LONGITUDINAL MOTION; LONGITUDINAL VELOCITY; STOCHASTIC ROBUSTNESS;

CONTROLLERS;

EID: 77958611837     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-7291     Document Type: Conference Paper

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