复杂电磁威胁环境下基于MSDBO算法的战机低空突防航迹规划
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河北水利电力学院

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V249.1;TP18

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国家自然科学基金项目面上项目(62273033),河北省教育厅科学研究项目资助(ZC2025095),沧州市自然科学基金(23241002014N);河北水利电力学院基本科研业务费项目(SYKY2308)


Low-altitude penetration trajectory planning for fighter aircraft based on MSDBO algorithm in complex electromagnetic threat environment
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    摘要:

    针对现代一体化防空体系下战机低空突防面临的雷达网探测、导弹拦截与复杂地形规避等多重威胁耦合问题,提出一种基于多策略融合改进蜣螂优化算法(multi-strategy improved dung beetle optimizer,MSDBO)的航迹规划方法。首先,建立基于Swerling I型目标探测概率的雷达威胁模型,综合考虑战机姿态角对雷达散射截面积的动态影响;其次,结合战机最大转弯角、爬升角和最小转弯半径等运动学硬约束,采用动态归一化方法设计多目标适应度函数;然后,针对标准蜣螂优化算法的不足,引入Tent-Logistic复合混沌初始化、非线性自适应权重、柯西-高斯混合变异和折射反向学习4种改进策略;最后,采用B样条曲线对航迹进行平滑处理。仿真结果表明,与标准蜣螂优化算法相比,所提算法规划的航迹长度缩短8.6%,威胁代价降低15.2%;与粒子群优化算法相比,航迹长度缩短18.5%,威胁代价降低37.1%;全航程累积被探测概率降低31.2%,突防生存概率提升至97.8%。

    Abstract:

    Aiming at the multi-threat coupling problem of radar network detection, missile interception and complex terrain avoidance faced by fighter aircraft in low-altitude penetration under modern integrated air defense system, a trajectory planning method based on multi-strategy improved dung beetle optimizer (MSDBO) is proposed. Firstly, a radar threat model based on Swerling I target detection probability is established, considering the dynamic influence of aircraft attitude angle on radar cross section. Secondly, combining the kinematic hard constraints such as maximum turning angle, climbing angle and minimum turning radius, a multi-objective fitness function is designed using dynamic normalization method. Thirdly, four improvement strategies including Tent-Logistic composite chaotic initialization, nonlinear adaptive weight, Cauchy-Gaussian hybrid mutation and refraction opposition-based learning are introduced to address the shortcomings of standard dung beetle optimizer. Finally, B-spline curve is used to smooth the planned trajectory. Simulation results show that compared with standard dung beetle optimizer, the trajectory length planned by MSDBO is reduced by 8.6% and the threat cost is reduced by 15.2%; compared with particle swarm optimization, the trajectory length is reduced by 18.5% and the threat cost is reduced by 37.1%; the cumulative detection probability throughout the flight is reduced by 31.2%, and the penetration survival probability is increased to 97.8%.

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  • 收稿日期:2025-12-06
  • 最后修改日期:2026-04-03
  • 录用日期:2026-04-05
  • 在线发布日期: 2026-06-12
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