系统工程与电子技术 ›› 2026, Vol. 48 ›› Issue (9): 3179-3190.doi: 10.12305/j.issn.1001-506X.2026.09.30

• 制导、导航与控制 • 上一篇    

基于自适应代价函数的再入滑翔飞行器意图推断

刘一辰1, 周池军2, 贺杨超1, 雷虎民2, 邵雷2, 王雪倩1   

  1. 1. 空军工程大学研究生院,陕西 西安 710051
    2. 空军工程大学防空反导学院,陕西 西安 710051
  • 收稿日期:2025-06-16 修回日期:2025-10-01 出版日期:2025-12-18 发布日期:2025-12-18
  • 通讯作者: 周池军
  • 作者简介:刘一辰(2000—),男,硕士研究生,主要研究方向为再入滑翔飞行器轨迹跟踪、轨迹预测
    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
    邵 雷(1982—),男,教授,博士,主要研究方向为再入滑翔目标轨迹预测、轨迹跟踪及空天拦截器制导控制与仿真
    王雪倩(2001—),女,博士研究生,主要研究方向为再入滑翔目标轨迹预测、智能算法
  • 基金资助:
    国家自然科学基金(62173339)资助课题

Intent inference of reentry glide vehicle based on adaptive cost function

Yichen Liu1, Chijun Zhou2, Yangchao He1, Humin Lei2, Lei Shao2, Xueqian Wang1   

  1. 1. Graduate School,Air Force Engineering University,Xi’an 710051,China
    2. Air and Missile Defense College,Air Force Engineering University,Xi’an 710051,China
  • Received:2025-06-16 Revised:2025-10-01 Online:2025-12-18 Published:2025-12-18
  • Contact: Chijun Zhou

摘要:

针对多禁飞区约束下的再入滑翔飞行器意图推断误判率高和所需时间较长的问题,提出一种基于自适应代价函数的意图推断方法。首先,分析基于常规特征参数构建的代价函数在多个禁飞区存在时的意图推断效果,并对其置信度进行评价,筛选出推断效果最好的意图代价函数。其次,在贝叶斯递推中引入鲁棒先验混合因子,根据飞行器的轨迹特性动态调节均匀分布与最低概率,有效防止了概率坍缩。最后,深度剖析飞行器、禁飞区和意图要地之间的相对态势关系,自适应融合角度维度和距离维度的意图代价函数,使得融合后的代价函数发挥更好的意图推断优势。仿真结果表明,与现有方法相比,本文所提方法对再入滑翔飞行器意图推断速度更快,能够获得更为可靠的意图推断结果。

关键词: 再入滑翔飞行器, 禁飞区, 代价函数, 贝叶斯定理, 意图推断

Abstract:

To address the issues of high misjudgment rates and excessively long inference time in intent inference for reentry glide vehicle under multiple no fly zone constraints, an intent inference method based on an adaptive cost function is proposed. Firstly, the effectiveness of intent inference using conventionally feature-based cost functions in multiple no fly zone scenarios is analyzed, and the confidence levels of these functions are evaluated to screen out the intent cost function with the best intent inference. Secondly, a robust prior mixing factor is introduced into Bayesian recursion. In light of the trajectory characteristics of the vehicle, it dynamically adjusts the uniform distribution and minimum probability, effectively preventing probability collapse. Finally, the relative situational relationships among the vehicle, no fly zones, and intended key regions of intent are analyzed in depth. The intent cost functions from angular and distance dimensions are adaptively fused, enabling the combined cost function to leverage superior intent inference capabilities. Simulation results demonstrate that compared to existing methods, the proposed approach achieves faster intent inference for reentry glide vehicle and delivers more reliable intent inference results.

Key words: reentry glide vehicle, no fly zone, cost function, Bayesian theorem, intent inference

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