DocumentCode
3133789
Title
Neural network based adaptive dynamic inversion flight control system design
Author
Lili ; Hua-min, Zhang
Author_Institution
Dept. of Aerial Instrum. & Electr. Eng., First Aeronaut. Inst. of Air Force, Xin Yang, China
Volume
1
fYear
2011
fDate
25-28 July 2011
Firstpage
135
Lastpage
137
Abstract
This paper introduces a neutral network(NN) based adaptive dynamic inversion flight control system. Super-maneuverable flight control law adapts nonlinear inversion design; on-line learning neural networks are implemented to compensate inversion errors due to modeling error or actuator faults. Simulation results show that through adaptively compensating inversion error by neutral networks, the limitation of needing accurate mathematical model in dynamic inversion method is released and the robustness of the whole system is greatly enhanced.
Keywords
adaptive control; aerospace control; control engineering computing; control system synthesis; neurocontrollers; nonlinear control systems; robust control; adaptive dynamic inversion flight control system; nonlinear inversion design; online learning neural networks; robustness; super-maneuverable flight control law; Adaptive systems; Aerodynamics; Aerospace control; Atmospheric modeling; Biological neural networks; Mathematical model; Nonlinear dynamical systems; adaptive control; dynamic inversion; flight control; neural network;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Control and Information Processing (ICICIP), 2011 2nd International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4577-0813-8
Type
conf
DOI
10.1109/ICICIP.2011.6008215
Filename
6008215
Link To Document