DocumentCode :
1662108
Title :
GP based flight control in the windshear
Author :
Imae, Joe ; Nakatani, Satoru ; Takahashi, Junya
Author_Institution :
Dept. of Mech. Eng., Iwate Univ., Morioka, Japan
Volume :
2
fYear :
1999
fDate :
6/21/1905 12:00:00 AM
Firstpage :
650
Abstract :
We deal with the flight control problem of a passenger aircraft encountering windshear during the landing process. First, we give a detailed description of the genetic programming (GP), which plays a key role in constructing robust flight controllers against windshear. Then, based on this GP, we propose a new design method, demonstrating its effectiveness through some numerical examples. Finally, we attack the landing-in-windshear problem by applying the proposed design method to this problem. Simulation is carried out with the parameters of the Boeing-727 type aircraft. No matter how strong the windshear is, the resulting robust controller shows good performance
Keywords :
aircraft control; genetic algorithms; multivariable control systems; optimal control; robust control; Boeing-727; design method; flight control; genetic programming; landing-in-windshear problem; passenger aircraft; robust flight controllers; windshear; Aerospace control; Aircraft; Control design; Design methodology; Differential equations; Genetic algorithms; Genetic programming; Robust control; Shape; Tree data structures;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems, Man, and Cybernetics, 1999. IEEE SMC '99 Conference Proceedings. 1999 IEEE International Conference on
Conference_Location :
Tokyo
ISSN :
1062-922X
Print_ISBN :
0-7803-5731-0
Type :
conf
DOI :
10.1109/ICSMC.1999.825337
Filename :
825337
Link To Document :
بازگشت