Three-Dimensional Flight Conflict Detection and Resolution Based on Particle Swarm Optimization

IF 0.1 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Weijun Pan, Liru Qin, Qinyue He, Yuanjing Huang
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引用次数: 0

Abstract

This paper presents a conflict detection and resolution method based on a velocity obstacle method for flight conflicts in a three-dimensional space. With the location and speed information of the two aircraft, the optimal relief strategy is obtained using particle swarm optimization. Aiming at the problem of excessive computational complexity in solving flight conflicts in a three-dimensional space with a cylindrical flight protection zone, an improved method for narrowing the search range is proposed to achieve a rapid solution by simplifying the complicated three-dimensional problem into a two-dimensional problem. The generality and flexibility of the method is effectively verified through simulations in flight conflict scenarios which almost cover all common situations. The experimental results show that the method can accurately determine the conflict time and generate the optimal relief strategy for different scenarios. The improved method of optimizing-search-range can significantly improve the computational efficiency, taking about 0.4 s to find the optimal solution, which can be used in real-time conflict resolution. The study provides a new solution for the flight conflict resolution problem.
基于粒子群优化的三维飞行冲突检测与解决
提出了一种基于速度障碍法的三维空间飞行冲突检测与解决方法。利用两架飞机的位置和速度信息,利用粒子群算法获得最优救援策略。针对在具有圆柱形飞行保护区的三维空间中求解飞行冲突计算量过大的问题,提出了一种改进的缩小搜索范围的方法,将复杂的三维问题简化为二维问题,实现了快速求解。通过对几乎涵盖所有常见情况的飞行冲突场景的仿真,有效验证了该方法的通用性和灵活性。实验结果表明,该方法能够准确地确定冲突时间,并针对不同场景生成最优救援策略。改进后的优化-搜索范围方法可以显著提高计算效率,找到最优解的时间约为0.4 s,可用于实时冲突解决。该研究为飞行冲突解决问题提供了一种新的解决方案。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aerospace America
Aerospace America 工程技术-工程:宇航
自引率
0.00%
发文量
9
审稿时长
4-8 weeks
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