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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2005, Vol. 26 ›› Issue (6): 720-725.

• 论文 • Previous Articles     Next Articles

Development of Nonlinear Flight Control Technology for Fighter Aircrafts

ZHU Jia-qiang1, GUO Suo-feng2, ZHU Ji-hong1, HU Chun-hua3   

  1. 1. State Key Laboratory of Intelligent Technology and Systems, Tsinghua University, Beijing 100084, China;2. College of Automation, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;3. School of Aerospace, Tsinghua University, Beijing 100084, China
  • Received:2004-09-02 Revised:2004-12-22 Online:2005-12-25 Published:2005-12-25

Abstract: Researches on nonlinear flight control of fighter aircrafts are surveyed. Technical development directions for future advanced fighter aircrafts are summarized and major fighter aircraft flight control designing approaches are introduced. Research activities on neural network based intelligent flight control are introduced particularly. It is pointed out that, as an important research direction, neural network based intelligent adaptive control will provide potential flight control schemes for advanced fighter aircrafts in the future.

Key words: flight control, nonlinear control, adaptive control, intelligent control, neural network

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