NDLI: Application of intelligence technology in super-maneuverable flight control

Content Provider	IEEE Xplore Digital Library
Author	Jie, L. Kai, L. Hang, X. Li, L.
Copyright Year	2008
Description	Author affiliation: The First Aeronautical Institute of Air Force (Jie, L.; Kai, L.; Hang, X.; Li, L.)
Abstract	This paper introduces the control strategy and method of non-linear dynamic inversion. Depending on the thought of dynamic inversion, the mathematical model of super-maneuverable aircraft is set up and the simulation curves are produced. Through analyzing the curves, we can draw out the feasibility and limitation of non-linear dynamic inversion.This paper introduces below contents :the feasibility of dynamic inversion in super-maneuverable flight; the modeling error and inversion error; the influence on super-maneuverable flight caused by uncertain factors. To solve above problems, the paper points out two kinds of methods. One is fuzzy self-adaptive technology. It describes the characteristic of fuzzy controller and points out its limitation that it can¿t be used to eliminate the error caused by uncertain factors. The other is neural network technology. It describes the dynamic inversion off-line neural network controller. On-line neural network controller eliminates error. At last the conclusion is gotten that neural network is more advantageous and the development direction of super-maneuverable flight.
Starting Page	1185
Ending Page	1188
File Size	508604
Page Count	4
File Format	PDF
ISBN	9781424416752
DOI	10.1109/RAMECH.2008.4690876
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2008-09-21
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Aerospace control Aerodynamics Nonlinear dynamical systems Neural networks State feedback Nonlinear equations Mathematical model Aircraft propulsion Fuzzy control Error correction fuzzy self-adaptive, neural network Super-maneuverable flight, dynamic inversion
Content Type	Text
Resource Type	Article

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