航空学报 > 2005, Vol. 26 Issue (6): 720-725

战斗机非线性飞行控制技术的研究与发展

朱家强1, 郭锁凤2, 朱纪洪1, 胡春华3   

  1. 1. 清华大学 智能技术与系统国家重点实验室, 北京 100084;2. 南京航空航天大学 自动化学院, 江苏 南京 210016;3. 清华大学 航天航空学院, 北京 100084
  • 收稿日期:2004-09-02 修回日期:2004-12-22 出版日期:2005-12-25 发布日期:2005-12-25

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

摘要: 战斗机非线性飞行控制技术研究综述。首先介绍战斗机技术发展走向,然后对当前主要战斗机飞行控制设计方案进行分析,并重点介绍神经网络在飞行控制中的应用研究。最后指出,基于神经网络的智能控制方案作为飞行控制的重要研究方向,将为未来先进战斗机飞行控制系统设计提供重要的解决方案。

关键词: 飞行控制, 非线性控制, 自适应控制, 智能控制, 神经网络

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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