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兵工学报 ›› 2023, Vol. 44 ›› Issue (9): 2580-2590.doi: 10.12382/bgxb.2022.1160

所属专题: 智能系统与装备技术

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弹群分布式一致误差约束自适应最优协同拦截方法

刘大卫1, 孙景亮2,3,*(), 龙腾2,3, 何镜1, 王晓悦1,2   

  1. 1 中国兵器科学研究院, 北京 100089
    2 北京理工大学 宇航学院, 北京 100081
    3 北京理工大学重庆创新中心, 重庆 401120
  • 收稿日期:2022-11-30 上线日期:2023-02-20
  • 通讯作者:
  • 基金资助:
    国家自然科学基金项目(62003036); 北京市自然科学基金项目(4214077); 北京理工大学青年教师学术启动计划项目(XSQD-202201005)

Distributed Adaptive Optimal Cooperative Interception Method for Missile Swarm with Synchronization Error Constraints

LIU Dawei1, SUN Jingliang2,3,*(), LONG Teng2,3, HE Jing1, WANG Xiaoyue1,2   

  1. 1 China Research and Development Academy of Machinery Equipment, Beijing 100089, China
    2 School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
    3 Beijing Institute of Technology Chongqing Innovation Center, Chongqing 401120, China
  • Received:2022-11-30 Online:2023-02-20

摘要:

为解决机动目标干扰下协同制导系统模型部分未知以及一致误差约束限制导致协同一致性差的问题,建立前馈补偿+反馈优化的复合协同制导架构,提出分布式自适应最优协同拦截制导方法。在前馈补偿部分,设计障碍Lyapunov函数非线性映射机制,补偿误差约束影响。设计权值自适应的神经网络观测器,实现对目标未知机动干扰的在线估计;在反馈优化部分,采用自适应动态规划技术设计虚拟控制量和实际控制量,将每一步中控制量设计转化为非线性耦合哈密顿-雅可比-贝尔曼(HJB)方程的求解问题。构建分布式自适应评价网络,设计残余误差驱动的评价网络权值自适应更新律,实现对HJB方程中最优代价函数的在线迭代求解。基于Lyapunov稳定性理论证明了非线性协同制导闭环系统的稳定性,确保了协同一致性误差的收敛性。数值仿真结果表明:新方法能够在保证拦截制导精度的同时将协同一致性误差降低至0.01s。

关键词: 协同拦截, 目标机动, 自适应动态规划, 误差约束, 自适应评价网络

Abstract:

To deal with the problem of poor synchronization for partial unknown nonlinear cooperative guidance system subject to synchronization error constraints caused by unknown maneuvering targets, a feedforward compensation+feedback optimization cooperative guidance framework is constructed. Then, a distributed adaptive optimal cooperative interception guidance method is proposed. In the feedforward compensation part, a nonlinear mapping mechanism is provided by designing a novel barrier Lyapunov function (BLF) for compensating the system effects of synchronization error constraints. To estimate the unknown nonlinear term caused by the maneuvering target, a neural network (NN) observer is built, in which the weight values are updated adaptively for estimating the target's unknown maneuvering disturbance. In the feedback optimization part, the virtual and actual control inputs are designed recursively by using the ADP technique, in which the control input in every backstepping process is transformed into the issue of solving the nonlinear coupled HJB equation. An adaptive critic network is built to solve the optimal cost function of the HJB equation online, in which a residual error based adaptive updating law of critic weight is derived. The stability of the nonlinear cooperative guidance closed-loop system is analyzed and the convergence of cooperative synchronization error is guaranteed theoretically based on the Lyapunov theory. The simulation results show that the synchronization error can be reduced to 0.01s while ensuring the interception precision with the proposed method.

Key words: cooperative interception, target maneuvering, ADP, error constraints, adaptive critic network

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