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基于约束人工势场法的弹载飞行器实时避障航迹规划

王伟 王华

王伟, 王华. 基于约束人工势场法的弹载飞行器实时避障航迹规划[J]. 航空动力学报, 2014, (7): 1738-1743. doi: 10.13224/j.cnki.jasp.2014.07.029
引用本文: 王伟, 王华. 基于约束人工势场法的弹载飞行器实时避障航迹规划[J]. 航空动力学报, 2014, (7): 1738-1743. doi: 10.13224/j.cnki.jasp.2014.07.029
WANG Wei, WANG Hua. Real-time obstacle avoidance trajectory planning for missile borne air vehicle based on constrained artificial potential field method[J]. Journal of Aerospace Power, 2014, (7): 1738-1743. doi: 10.13224/j.cnki.jasp.2014.07.029
Citation: WANG Wei, WANG Hua. Real-time obstacle avoidance trajectory planning for missile borne air vehicle based on constrained artificial potential field method[J]. Journal of Aerospace Power, 2014, (7): 1738-1743. doi: 10.13224/j.cnki.jasp.2014.07.029

基于约束人工势场法的弹载飞行器实时避障航迹规划

doi: 10.13224/j.cnki.jasp.2014.07.029
详细信息
    作者简介:

    王伟(1975-),女,河北保定人,博士生,主要研究方向为弹载飞行器设计。

  • 中图分类号: V249

Real-time obstacle avoidance trajectory planning for missile borne air vehicle based on constrained artificial potential field method

  • 摘要: 针对弹载飞行器飞行高度低、需实时避障的需求,提出了一种三维约束人工势场法用于弹载飞行器的实时避障航迹规划.该方法将人工势场法扩展到三维空间,增加了一个势场函数——高度调节势场函数,并将弹载飞行器的动力学约束条件引入人工势场法中.该方法继承了传统人工势场法计算速度快、占用内存少的优点,并能保证所规划航迹的可飞性.仿真结果显示约束人工势场法相比于传统人工势场法,具有以下优势:所规划的航迹更具有可飞性;可明显减弱在障碍物附近的抖动现象;可显著改善在狭窄通道中的摆动现象;不易陷入局部最小点.

     

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出版历程
  • 收稿日期:  2013-04-09
  • 刊出日期:  2014-07-28

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