Novel Particle Swarm Optimization Guidance for Hypersonic Target Interception with Impact Angle Constraint
Author:
Affiliation:
1. Department of Ordnance Engineering, Naval University of Engineering, Wuhan 430030, China
2. Naval Equipment Department, Beijing 100071, China
Abstract
Funder
Naval University of Engineering
Publisher
Hindawi Limited
Subject
Aerospace Engineering
Link
http://downloads.hindawi.com/journals/ijae/2022/7615644.pdf
Reference23 articles.
1. An adaptive reaching law based three-dimensional guidance laws for intercepting hypersonic vehicle;Y. Si;International Journal of Innovative Computing, Information and Control,2017
2. Integration of a fuzzy guidance-control system for a command interceptor against hypersonic target;Y. Z. Elhalwagy;IECON'01. 27th Annual Conference of the IEEE Industrial Electronics Society (Cat. No.37243),2001
3. Guidance strategy with impact angle constraints based on pure proportional navigation;K.-B. Li;Acta Aeronauticaet Astornautica Sinica,2020
4. Three-dimensional united biased proportional navigation law for interception of maneuvering targets with angular constraint
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. Computational Optimal Impact Angle Control Guidance Laws Weighted by Arbitrary Functions;International Journal of Aerospace Engineering;2023-01-05
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