摘要
介绍了一种基于阿波罗尼奥斯圆(Apollonius circle)理论的无人机追逃问题求解方法。首先介绍了阿波罗尼奥斯圆相关理论,然后构建了2个单无人机追逃问题和多无人机追逃问题的数学模型,并对2种模型下逃跑无人机的逃逸条件和追捕无人机的追捕条件进行了求解,最后通过仿真,设定实验场景,求出了逃跑无人机的绝对逃逸区域,验证了所构建模型的正确性和有效性。
A method is introduced to solve the problem of UAV pursuit and evasion based on the theory of Apollonius circle.First of all,the related theory of Apollonius circle is introduced,and two mathematical models are constructed:two single-UAV pursuit and evasion problems and multiple UAV pursuit and evasion problems.Then,the evasion conditions of the evasion UAV and the pursuit conditions of the pursuit UAV under the two models are solved.Finally,a certain experimental scene is set,and through simulation,the absolute evasion area of the evasion drone is obtained,which verifies the correctness and effectiveness of the constructed model.
作者
张澄安
邓文
王李瑞
龙淼
姚怡舟
Zhang Cheng'an;Deng Wen;Wang Lirui;Long Miao;Yao Yizhou(National Key Laboratory of CEMEE,School of Electronic Science,National University of Defense Technology,Changsha 410073,Hunan,China;Unit 75836 of PLA,Guangzhou 510036,Guangdong,China)
出处
《航天电子对抗》
2021年第5期40-43,48,共5页
Aerospace Electronic Warfare
关键词
无人机
追逃
阿波罗尼奥斯圆
约束条件
UAV
pursuit and evasion
Apollonius circle
constraint condition
