宇航学报

宇航学报 ›› 2021, Vol. 42 ›› Issue (3): 333-343.doi: 10.3873/j.issn.1000-1328.2021.03.008

• 制导、导航、控制与电子 • 上一篇    下一篇

高超声速目标拦截末段交战窗口快速生成方法

梁子璇，郭栋，朱圣英，任章   

  1. 1. 北京理工大学宇航学院，北京 100081；2. 深空自主导航与控制工信部重点实验室，北京 100081；3. 中国运载火箭技术研究院，北京 100076；4. 北京航空航天大学自动化科学与电气工程学院，北京 100191

  • 收稿日期:2020-04-08 修回日期:2020-05-28 出版日期:2021-03-15 发布日期:2021-03-15
  • 基金资助:
    国家自然科学基金（61803008，61333011）

Rapid Generation of Terminal Engagement Window for Interception of Hypersonic Targets

LIANG Zi xuan, GUO Dong, ZHU Sheng ying, REN Zhang   

  1. 1. School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China; 2. Key Laboratory of Autonomous Navigation and Control for Deep Space Exploration, Ministry of Industry and Information Technology, Beijing 100081, China;3. China Academy of Launch Vehicle Technology, Beijing 100076, China; 4. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, China
  • Received:2020-04-08 Revised:2020-05-28 Online:2021-03-15 Published:2021-03-15

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摘要： 针对高超声速目标拦截问题，提出了拦截器的末段交战窗口(TEW)快速生成方法，该窗口表征了所有可行的末段交战阵位。首先，针对高超声速非机动目标建立了解析形式的拦截条件。在此基础上，针对非机动目标和机动目标，依次推导了TEW边界的解析方程。同时，根据拦截器的最小和最大初始航向角，定义并计算了TEW内所有位置的可控裕度。最后，通过对高超声速目标TEW仿真，验证了所提出方法的有效性，并分析了TEW边界和可控裕度的影响因素。与传统数值方法相比，本文解析方法生成的TEW边界一致，但计算耗时大幅减小，具有在线使用的潜力。此外，仿真结果也表明，当目标信息存在测量误差时，所提出的TEW生成方法依然有效。

关键词: 拦截器, 高超声速目标；末段交战窗口；拦截条件；机动目标

Abstract: In this paper, a generation method of terminal engagement window (TEW), which describes the set of feasible engagement positions in the terminal guidance phase, is developed for the interception of hypersonic targets. Firstly, an analytical interception condition is established. On this basis, the analytical solutions of the TEW boundary are successively derived for the non maneuvering and maneuvering targets. Then, a controllable margin is defined and calculated for each position in the TEW according to the interceptor’s minimum and maximum initial heading angles. Finally, the TEW generation method is verified by simulations, and the influence factors are analyzed for the TEW boundary together with the controllable margin. Compared with the traditional numerical approaches, the proposed analytical approach has the consistent results but much lower computational cost, and thus is more capable to generate a TEW onboard. The results also indicate that the generation method is still effective when the measurement errors of the target exist.

Key words: Interceptor, Hypersonic target, Terminal engagement window, Interception condition, Maneuvering target

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