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一种同时满足攻击角度和时间的航迹规划方法

  • 姚冬冬 ,
  • 王晓芳 ,
  • 田震
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  • 北京理工大学宇航学院,北京 100081

姚冬冬(1993-),男,吉林长春人,硕士研究生,研究方向:飞行器航迹规划,飞行器制导与控制。

收稿日期: 2019-01-26

  网络出版日期: 2025-05-20

A Cooperative Path Planning with Constraints of Impact Time and Impact Angle

  • YAO Dongdong ,
  • WANG Xiaofang ,
  • TIAN Zhen
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  • School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China

Received date: 2019-01-26

  Online published: 2025-05-20

摘要

为了进行多导弹从指定方向同时攻击目标的协同航迹规划。文中基于稀疏A*算法,根据导弹飞行约束和轨迹圆滑方式扩展节点;通过增加控制点并调整代价函数实现攻击角度约束;假设多导弹速度相同,通过选取期望长度重新规划其他航迹;对航迹节点进行时空安全检测与重置,避免了弹间的碰撞;最后进行轨迹平滑,得到满足飞行和攻击约束的可飞航迹。仿真结果表明了算法的有效性。

本文引用格式

姚冬冬 , 王晓芳 , 田震 . 一种同时满足攻击角度和时间的航迹规划方法[J]. 弹箭与制导学报, 2019 , 39(3) : 111 -114 . DOI: 10.15892/j.cnki.djzdxb.2019.03.025

Abstract

In order to carry out coordinated flight planning of multiple missiles simultaneously attacking targets from a specified direction. Based on the sparse A algorithm, the node is extended according to the missile flight constraint and the trajectory smoothing method; the angle to attack constraint is realized by increasing the control point and adjusting the cost function; assuming that the multi-missile speed is the same, re-planning other tracks by selecting the desired length; the nodes perform time-space security detection and resetting to avoid collisions among the missiles; finally, the trajectory is smoothed to obtain flightable tracks that meet the constraints of flight and attack. The simulation results show the effectiveness of the algorithm.

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