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基于A*算法的实时航迹规划方法研究
引用本文:史宗鹏,杜萍,毕义明. 基于A*算法的实时航迹规划方法研究[J]. 海军工程大学学报, 2006, 18(5): 79-82
作者姓名:史宗鹏  杜萍  毕义明
作者单位:第二炮兵工程学院,陕西,西安,710025
摘    要:根据巡航导弹实时航迹规划时效性强、弹载计算设备的运算速度和内存容量有限等特点,将巡航导弹的机动性能约束与规划空间的划分结合起来,构造了一个较小的搜索空间,然后在此缩小了的搜索空间内利用A*算法具有的启发式特点,可在有效时间内搜索到满足要求的可行航迹.最后,通过一个例子对A*算法进行了验证.

关 键 词:巡航导弹  实时航迹规划方法  A*算法  规划空间
文章编号:1009-3486(2006)05-0079-04
修稿时间:2006-07-18

A study of real-time route planning approach based on A* algorithm
SHI Zong-peng,DU Ping,BI Yi-ming. A study of real-time route planning approach based on A* algorithm[J]. Journal of Naval University of Engineering, 2006, 18(5): 79-82
Authors:SHI Zong-peng  DU Ping  BI Yi-ming
Abstract:According to the strict time-efficiency of real-time route planning for cruise missile and the finitude of the operation speed and memory capability of the computer on a cruise missile,this paper analyzes the maneuverability restriction of the cruise missile and the partition of planning space,constructs a lesser searching space,and then by using A~* algorithm in the lesser searching space,the feasible route can be obtained to meet the requirement in the availability time.Finally,an example is used to check A~* algorithm.
Keywords:cruise missile  real-time route planning approach  A~* algorithm  planning space
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