Air Defense Interception Plan Generation Method Based on Modified A* Optimization Algorithm

Author:

Song Xiaocheng1,Li Zhi1,Feng Shuting1,Li You2,Sun Liang3,Jiang Jingjing4ORCID

Affiliation:

1. Department of Beijing Institute of Electronic Engineering, China Aerospace Science and Industry Corporation Co., Ltd., Beijing 100143, China

2. School of Aerospace Science and Technology, Xidian University, Xi’an 710126, China

3. School of Intelligence Science and Technology, University of Science and Technology Beijing, Beijing 100083, China

4. Department of Aeronautical and Automotive Engineering, Loughborough University, Loughborough LE11 3TU, UK

Abstract

Aiming at the air defense task requirements for an enemy’s large-scale aircraft attack, this paper presents a plan generation algorithm which can quickly give an interception scheme. The main contribution of this paper is the modification of the standard A* algorithm and its combination of the optimization algorithm and air-defence mission. Firstly, the enemy’s attack weapon and our defense platform are modeled, and kinetic equations and interception efficiency functions are constructed, and the intercepted criterions are established. Then, the interception-cost mixed optimal function is established to clarify the system optimization objective. Secondly, aiming at the characteristics of strong time sensitivity of air defense interception, a modified A* optimization algorithm with fast convergence characteristics is used to solve the optimization problems, the standard A* algorithm is modified and the optimal air defense interception plan under the condition of mixed performance index is given. Finally, the proposed method is verified by numerical simulations.

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

MDPI AG

Subject

Electrical and Electronic Engineering,Computer Networks and Communications,Hardware and Architecture,Signal Processing,Control and Systems Engineering

Reference20 articles.

1. Hughes, T.L., and McFarland, M.B. (2000, January 14–17). Integrated missile guidance law and autopilot design using linear optimal control. Proceedings of the AIAA Guidance, Navigation, and Control Conference, AIAA, Denver, CO, USA.

2. Some problems about anti-TBM disposition;Liu;Syst. Eng. Electron.,2001

3. Effective deployment area of the surface to air missile weapon system intercepting tactical ballistic missile;Bai;Mod. Def. Technol.,2003

4. Optimization of anti-TBM disposition;Liu;Syst. Eng. Theory Pract.,2002

5. Optimization of the regional air defense disposition based on genetic algorithms;Liu;Syst. Eng. Electron.,2003

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Planning for Air Defense Operations Based on Simulated Annealing Algorithm;2023 2nd International Conference on Machine Learning, Cloud Computing and Intelligent Mining (MLCCIM);2023-07-25

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3