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流体力学、飞行力学与发动机

高超声速飞行器制导与控制研究现状及发展趋势

方洋旺1,柴栋2,毛东辉3,张磊2   

  1. 1. 陕西省西安市空军工程大学工程学院二系
    2. 空军工程大学航空航天工程学院
    3. 空军工程大学航空航天工程学院研4队
  • 收稿日期:2014-01-01 修回日期:2014-03-22 出版日期:2014-04-01 发布日期:2014-04-01
  • 通讯作者: 柴栋
  • 基金资助:
    西北工业大学基础研究基金;学校级项目

Status and Development Trend of the Guidance and Control for Hypersonic Vehicle

  • Received:2014-01-01 Revised:2014-03-22 Online:2014-04-01 Published:2014-04-01
  • Contact: Dong CHAI

摘要: 制导与控制技术是发展高超声速飞行器的关键技术,同时也是控制学科研究的热点问题,许多先进控制理论在此领域得到应用。分析了吸气式高超声速飞行器动力学模型非线性、强耦合和不确定性等特点,指出高超声速飞行器制导与控制技术面临的挑战。在综述国内外研究成果的基础上,对吸气式高超声速飞行器制导与控制中基于线性化的非线性控制方法和直接针对非线性模型的控制方法分类讨论,分析了尚待解决的问题和不足。最后,结合吸气式高超声速飞行器鲁棒性、自适应性和智能化的目标,从面向机动目标制导律、高速目标拦截器制导律、全空域机动飞行控制和先进智能控制理论等方面展望了此领域研究的发展趋势。

Abstract: Guidance and control technique is one of the key technologies of hypersonic vehicles, and it is also a focus issue in control discipline, which many advanced control theories have been applied in the field. The paper analyzes the nonlinearity, strong couplings, uncertainties and other characteristics of the air-breathing hypersonic vehicle’s dy-namic model, and points out the challenges of guidance and control technique for hypersonic vehicle. Then, based on combing the domestic and foreign research results, the theories and approaches for this issue are discussed particularly by classification, including nonlinear control based on linearization and nonlinear control directly against nonlinear model. In addition, the unsolved problems and deficiencies in this field are analyzed by reviewing existing literature. Finally, combined with the goal of robustness, adaptability and intellectuality for the air-breathing hypersonic vehicle, the development tendency is suggested in the following four aspects: guidance law for tracking maneuvering target, guidance law of interceptor against hypersonic target, maneuvering control in all-aerospace and advanced intelligent control theories.

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