基于PSO-hpRPM算法的滑翔制导炮弹弹道优化
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TJ413

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国家自然科学基金项目(62203191);基础加强计划技术领域基金项目(2023JCJQJJ0357);江苏省高等学校基础科学(自然科学)研究面上项目(22KJB590001);国防科技重点实验室基金项目(2022JCJQL06105).


Trajectory optimization of glide guidance projectile based on PSO-hpRPM hybrid algorithm
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    摘要:

    针对滑翔制导炮弹在坏境高动态、状态强耦合等复杂多约束情况下弹道优化效率低、优化效果不理想等问题, 提出一种基于粒子群-hp自适应Radau伪谱(PSO-hpRPM)算法的滑翔制导炮弹弹道优化方法, 该方法融合PSO算法全局搜索能力强和hpRPM算法局部优化能力出色的特点, 能够解决滑翔制导炮弹在复杂多约束情况下的弹道优化问题. 首先, 建立滑翔制导炮弹动力学模型和弹道优化问题的约束条件和目标函数; 然后, 分别采用hpRPM、PSO和PSO-hpRPM方法进行滑翔弹道优化求解, 并对3种方法进行对比研究; 最后, 为了进一步验证所提出算法的优越性, 采用灰狼优化算法(GWO)、鲸鱼(WOA)与hpRPM算法相结合, 设计GWO-hpRPM算法和WOA-hpRPM算法, 并对3种混合优化算法进行仿真对比研究. 研究结果表明: 所提出PSO-hpRPM算法在同时满足复杂多约束条件下, 优化得到的最远滑翔弹道射程为70170.75 m, 平均迭代收敛步数为6.6步, 综合性能较其他算法更佳, 优化效果良好.

    Abstract:

    Aiming at the problems of the low trajectory optimization efficiency and unsatisfactory optimization effect of glide guided projectile under complex and multi-constraint conditions such as high dynamic environment and strong state coupling, a trajectory optimization method of glide guided projectile based on particle swarm optimization-hp adaptive Radau pseudospectral method(PSO-hpRPM) algorithm is proposed. This method combines the strong global search ability of the PSO algorithm and the excellent local optimization ability of the hpRPM algorithm to solve the trajectory optimization problem of glide-guided projectiles under complex and multi-constraint conditions. Firstly, the constraints and objective functions of glide-guided projectile dynamics model and trajectory optimization problem are established. Then, hpRPM, PSO and PSO-hpRPM methods are used to optimize glide trajectory, and the three methods are compared. Finaly, to further validate the superiority of the proposed algorithm, we integrate the grey wolf optimization(GWO) algorithm, the whale optimization algorithm(WOA), with the hpRPM algorithm, respectively. We then conduct simulations to compare the performance of these three hybrid optimization algorithms: PSO-hpRPM, GWO-hpRPM, and WOA-hpRPM. The results show that the optimized PSO-hpRPM algorithm has a maximum glide range of 70170.75 m and an average iterative convergence of 6.6 steps under complex and multi-constraint conditions. The comprehensive performance is better than other algorithms and the optimization effect is good.

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管军,叶双慧,易文俊.基于PSO-hpRPM算法的滑翔制导炮弹弹道优化[J].控制与决策,2025,40(5):1733-1741

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  • 收稿日期:2024-09-09
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  • 在线发布日期: 2025-04-15
  • 出版日期: 2025-05-20
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