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考虑规避与突防的高超声速飞行器智能容错制导控制一体化设计方法

武天才,王宏伦,任斌,刘一恒,吴星雨,严国乘   

  1. 北京航空航天大学自动化科学与电气工程学院
  • 收稿日期:2023-09-19 修回日期:2024-01-13 出版日期:2024-01-15 发布日期:2024-01-15
  • 通讯作者: 王宏伦
  • 基金资助:
    国家自然科学基金;北京航空航天大学博士研究生卓越学术基金;北京航空航天大学未来空天技术学院/高等理工学院卓越研究基金;航空科学基金

Learning-based integrated fault-tolerant guidance and control method for hypersonic vehicles considering avoidance and penetration

  • Received:2023-09-19 Revised:2024-01-13 Online:2024-01-15 Published:2024-01-15
  • Supported by:
    National Natural Science Foundation of China;Academic Excellence Foundation of BUAA, China for PhD Students;Outstanding Research Project of Shen Yuan Honors College, BUAA;Aeronautical Science Foundation of China

摘要: 针对再入过程中的禁飞区规避和拦截弹躲避问题,本文提出一种考虑规避与突防的高超声速飞行器智能容错制导控制一体化设计方法。首先,在纵向制导中,为提升飞行器的制导性能,基于制导控制一体化设计思想,本文采用包含姿态容错控制系统在内的飞行器六自由度模型进行待飞航程的预测;针对随之产生的计算耗时问题,进一步采用深度网络进行预测环节的拟合,来提升算法的实时性;接着,在侧向制导中,为解决禁飞区规避和拦截弹躲避问题,引入扰动流体算法进行考虑威胁因素的飞行器期望航向角计算,并结合航向角误差走廊和倾侧角翻转逻辑进行侧向制导指令的求取,使飞行器具备规避与突防能力;然后,考虑到飞行环境的复杂性、飞行器再入段机动能力的差异性以及姿态容错控制系统动态特性对制导性能的影响,结合深度强化学习算法进行智能体训练,使其可根据飞行器实时状态进行扰动流体算法参数的在线决策,提升所提方法的有效性和适应能力。最后,由半物理对比仿真和蒙特卡洛仿真结果可得,所提方法可达到较强的规避、突防与制导性能。

关键词: 高超声速飞行器, 制导控制一体化, 规避与突防, 深度强化学习

Abstract: Aiming at the problem of no-fly zone and interceptor avoidance during reentry phase, a learning-based integrated fault-tolerant guidance and control method for hypersonic vehicles considering avoidance and penetration is proposed. The proposed method is based on the idea of separate longitudinal and lateral guidance design in traditional predic-tive correction guidance methods. First, in longitudinal guidance, to improve the guidance performance of the vehicle, based on the integrated design concept of guidance and control, the six degree of freedom model of the vehicle, in-cluding the attitude fault-tolerant control system, is adopted for predicting the range-to-go. In view of the resulting cal-culation time-consuming problem, the deep network is further used to fit the predicting process to improve the real-time performance of the algorithm. Then, in lateral guidance, to solve the problem of avoiding no-fly zone and inter-ceptor, the interfered fluid dynamical system is introduced to calculate the expected heading angle of the vehicle con-sidering the threat factors, and the heading angle error corridor and the flip logic of the bank angle are combined to obtain the command, so that the vehicle has the ability of avoidance and penetration. Then, considering the complexi-ty of flight environment, the difference of maneuvering ability of vehicle during reentry phase, and the influence of dy-namic characteristics of attitude control system on guidance performance, the deep reinforcement learning algorithm is combined to conduct agent training, so that it can make online decisions on key parameters of algorithm according to the real-time state of vehicle, and improve the effectiveness and adaptability of the proposed guidance method. Finally, the results of semi-physical comparison simulation and Monte Carlo simulation show that the proposed meth-od can achieve strong avoidance, penetration and guidance performance.

Key words: Hypersonic vehicle, Integrated guidance and control, Avoidance and penetration, Deep reinforcement learning

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