系统工程与电子技术 ›› 2025, Vol. 47 ›› Issue (8): 2715-2726.doi: 10.12305/j.issn.1001-506X.2025.08.29

• 制导、导航与控制 • 上一篇    

基于最小代价准则的再入滑翔制导方法

姬博洋, 李炯, 贺杨超, 叶继坤, 雷虎民   

  1. 空军工程大学防空反导学院,陕西 西安 710051
  • 收稿日期:2024-10-14 出版日期:2025-08-25 发布日期:2025-09-04
  • 通讯作者: 叶继坤
  • 作者简介:姬博洋(2001—),男,博士研究生,主要研究方向为再入滑翔目标轨迹生成、空天拦截器制导控制与仿真、智能博弈
    李 炯(1980—),男,副教授,博士,主要研究方向为再入滑翔目标轨迹预测、轨迹跟踪、空天拦截器制导控制与仿真
    贺杨超(1999—),男,博士研究生,主要研究方向为再入滑翔目标轨迹预测、轨迹跟踪、智能算法
    雷虎民(1960—),男,教授,博士,主要研究方向为再入滑翔目标轨迹预测、空天拦截器制导控制与仿真
  • 基金资助:
    国家自然科学基金(62173339)资助课题

Reentry gliding vehicle guidance method based on min-cost criterion

Boyang JI, Jiong LI, Yangchao HE, Jikun YE, Humin LEI   

  1. Air and Missile Defense College,Air Force Engineering University,Xi’an 710051,China
  • Received:2024-10-14 Online:2025-08-25 Published:2025-09-04
  • Contact: Jikun YE

摘要:

针对再入滑翔飞行器(reentry gliding vehicle,RGV)规避禁飞区的问题,提出一种基于最小代价准则的RGV制导方法。基于图论思想,引入规避时机判断准则,实现制导逻辑和规避逻辑的动态切换。在制导逻辑中,依据距离目标点的剩余航程设计分段式航向角偏差角走廊,提高制导精度。在规避逻辑中,设计规避策略和补偿策略。规避时统一量化飞行器的规避代价和制导代价,依据最小代价准则决定倾侧角符号,同时为降低能量损耗,求解恰好规避时的倾侧角幅值实现倾侧角的自适应变化。为避免倾侧角符号的频繁偏转,对航向角偏差走廊进行自适应补偿。该制导方法旨在解决规避任务与制导任务相冲突、多禁飞区叠加影响时的规避决策问题。仿真结果表明,和传统方法相比所提制导方法可以实现最小代价的多禁飞区规避,且具有更高的制导精度,算法具有一定的鲁棒性。

关键词: 预测-校正法, 最小代价准则, 自适应航向角偏差走廊, 禁飞区规避

Abstract:

Aiming at the no-fly zone avoiding problem of reentry gliding vehicle (RGV), a RGV guidance method based on the min-cost criterion is proposed. Based on the idea of graph theory, it introduces the judgement criterion of avoidance timing to achieve dynamic switching between guidance logic and avoidance logic. In the guidance logic, the segmented heading angle deviation corridor is designed based on the remaining range from the target point to improve the guidance accuracy. In the avoidance logic, the avoidance strategy and compensation strategy are designed. The avoidance cost and guidance cost of vehicle are quantified uniformly during avoidance, and the sign of bank angle is determined by the min-cost criterion. In order to reduce the energy loss, the bank angle changes adaptively by solving the amplitude of the bank angle at the time of just-avoidance. The heading angle deviation corridor is compensated adaptively to avoid the frequent reversal of the bank angle. This guidance method is designed to solve the decision problem when the avoidance task conflicts with the guidance task and when the multiple no-fly zones superimpose effects. Simulation results show that compared with the traditional methods, the proposed guidance method can avoid multiple no-fly zones with min-cost. The algorithm has higher guidance accuracy and good robustness.

Key words: prediction-correction method, min-cost criterion, adaptive heading angle deviation corridor, no-fly zone avoidance

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