GA based design of sliding mode control law for hypersonic vehicle

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

Volumn 35, Issue 9, 2009, Pages 1144-1147

  Li, Huifeng ^a   Wang, Jian ^a   Sun, Wenchong ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Feedback linearization; Hypersonic; Sliding mode control; Stochastic robustness

Indexed keywords

AFFINE SYSTEMS; CONTROL PARAMETERS; DESIGN PROCESS; FLIGHT CONTROL; GENERIC HYPERSONIC VEHICLES; HYPERSONIC; HYPERSONIC VEHICLES; INPUT-OUTPUT FEEDBACK LINEARIZATION; NON-LINEAR MODEL; PARAMETER OPTIMIZATION; PARAMETER UNCERTAINTY; SIX-DOF; SLIDING MODES; STOCHASTIC ROBUSTNESS; STRUCTURE DESIGN; UNIFORM DISTRIBUTION;

CONTROL SYSTEM ANALYSIS; FEEDBACK; FEEDBACK LINEARIZATION; FLIGHT CONTROL SYSTEMS; GENETIC ALGORITHMS; GENETIC ENGINEERING; HYPERSONIC AERODYNAMICS; NONLINEAR CONTROL SYSTEMS; ROBUST CONTROL; ROBUSTNESS (CONTROL SYSTEMS); SIMULATORS; SLIDING MODE CONTROL; STOCHASTIC SYSTEMS; STRUCTURAL DESIGN; STRUCTURAL OPTIMIZATION;

PROCESS CONTROL;

EID: 70350592485     PISSN: 10015965     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (4)

1. Heller M, Sachs G. Flight dynamics and robust control of a hypersonic test vehicle with ramjet propulsion[R]. AIAA-98-1521, 1998
2. Wu S F, Engelen C J H, Babuska R, et al. Intelligent flight controller design with fuzzy logic for an atmospheric re-entry vehicle[R]. AIAA-2000-0174, 2000
3. Feng Yong, Zheng Xuemei, Bao Sheng. Terminal sliding mode decomposed control of multivariable linear uncertain systems[J]. Control Theory and Applications, 2004, 21(1): 11-16(in Chinese)
4. Wang Qian, Stengel R. Robust nonlinear control of a hypersonic aircraft[R]. AIAA-99-4000, 1999