DocumentCode
406154
Title
Gain scheduled model following control of flight control system based on neural network
Author
Xinmin, Dong ; Zhiguo, Xiong ; Qin, Liu
Author_Institution
Dept. of Aeronaut. Control Eng., Eng. Inst. of the Air Force Eng. Univ., Xi´´an, China
Volume
1
fYear
2003
fDate
14-17 Dec. 2003
Firstpage
301
Abstract
Gain scheduling control method is widely used in flight control system, but the designing process is time-consuming. This paper introduces a kind of gain scheduled model following control method based on neural network. Using this method, all the parameters in flight controller can be computed automatically. The structure of controller and the principles of selecting referenced model are presented. At the same time, conditions of perfect model following are given and proved. The controller of a fly by wire system in full flight envelope is realized by using BP neural network. Finally, the closed loop system in several typical states is simulated. The simulation results show that the gain scheduled model following control method can satisfy the requirements of flying qualities in longitudinal short period motion.
Keywords
aerospace control; backpropagation; closed loop systems; control system synthesis; neurocontrollers; scheduling; BP neural network; closed loop system; flight control system; flight envelope; fly by wire system; gain scheduling control method; referenced model; time-consuming design process; Aerospace control; Aerospace engineering; Aircraft; Automatic control; Control systems; Design engineering; Design methodology; Force control; Neural networks; Processor scheduling;
fLanguage
English
Publisher
ieee
Conference_Titel
Neural Networks and Signal Processing, 2003. Proceedings of the 2003 International Conference on
Conference_Location
Nanjing
Print_ISBN
0-7803-7702-8
Type
conf
DOI
10.1109/ICNNSP.2003.1279270
Filename
1279270
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