Robust control system design using simulated annealing

Journal of Guidance, Control, and Dynamics

Volumn 25, Issue 2, 2002, Pages 267-274

  Motoda, Toshikazu ^a   Stengel, Robert F ^b   Miyazawa, Yoshikazu ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

^b Princeton University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLIGHT DYNAMICS; MONTE CARLO METHODS; PROBABILITY; SIMULATED ANNEALING;

FLIGHT CONTROL SYSTEMS;

ROBUSTNESS (CONTROL SYSTEMS);

EID: 0036494188     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4878     Document Type: Article

References (19)

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12. Fine tuning of aircraft control laws using Pro-MATLAB software
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14. Flight testing of ALFLEX guidance, navigation, and control system