多约束条件下战斗机三维路径规划问题

Ping Yang, Bing Xiao, Xin Chen, LiangLiang Guo
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引用次数: 0

摘要

航迹规划是保证飞行任务安全、高效的重要组成部分,对战斗机来说尤其如此。为了提高战斗机的作战效能,必须考虑如何避开危险源和地形障碍物,降低燃油消耗,并利用飞机自身性能来完成任务目标。在现代战场环境下,最短路径不仅是飞机规划的唯一标准,还包括对飞机的威胁程度、燃油消耗、任务完成时间、最小转弯半径等因素。在本文中,作者提出了一种将这些因素纳入改进粒子群算法的战斗机多约束路径规划方法。作者将三维地形、威胁源、燃料消耗和任务时间的约束转换为聚合适应度函数。作者构造了一个极限曲率矩阵来评价所生成路径的可行性。在粒子群算法中引入了一种基于激活函数的参数自适应调整策略。每个约束的权重根据实际需求确定。实验结果表明,该方法能有效地规划出满足要求的最优路径。与其他改进粒子群算法相比,该方法具有更高的最优搜索效率和更好的收敛效果。作者还提供了任务能耗、任务时间、飞行速度等重要参数的最优值,以支持整体任务规划。该方法具有一定的实际应用价值。
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3D path planning problem for fighter aircraft with multiple constraints
Abstract Path planning is a crucial component for ensuring the safety and efficiency of flight missions, especially for fighter aircraft. To enhance the combat effectiveness of fighter aircraft, it is important to consider how to avoid danger sources an terrain obstacles, reduce fuel consumption, and utilize the aircraft's own performance to accomplish the mission objectives. In the modern battlefield environment, the shortest path is not the only criterion for planning, but also other factors such as the threat level to the aircraft, fuel consumption, mission completion time, and minimum turning radius. In this paper, the authors propose a multi‐constraint path planning method for fighter aircraft that incorporates these factors into an improved particle swarm algorithm. The authors transform the constraints of three‐dimensional terrain, threat source, fuel consumption, and mission time into an aggregated fitness function. The authors construct a limit curvature matrix to evaluate the feasibility of the generated path. The authors also introduce an adaptive adjustment strategy based on the activation function for the parameters in the particle swarm algorithm. The weights of each constraint are determined according to the actual demand. The experiment results show that the authors’ method can efficiently plan the optimal path that satisfies the requirements. Compared with other improved particle swarm algorithms, the authors’ method has higher optimal search efficiency and better convergence effect. The authors also provide optimal values for important parameters such as mission energy consumption, mission time, flight speed and others to support the overall mission planning. The authors’ method has a certain practical application value.
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