Optimal Fixed-Interval Integrated Guidance-Control Laws for Hit-to-Kill Missiles
Author:
Affiliation:
1. Optimal Synthesis Inc.
2. Naval Surface Warfare Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-5579
Reference17 articles.
1. Integrated Guidance-Control Systems for Fixed-Aim Warhead Missiles
2. Integrated design of agile missile guidance and autopilot systems
Cited by 16 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. Novel integrated guidance and control design for a three-stage satellite carrier using model-free adaptive control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-03-27
2. Design of integrated Guidance and control system in the pitch channel using observer based chattering free sliding mode theory;Journal of Control;2020-05-01
3. Adaptive fin failures tolerant integrated guidance and control based on backstepping sliding mode;Transactions of the Institute of Measurement and Control;2020-01-10
4. Optimal Error Dynamics in Missile Guidance;Optimal Guidance and Its Applications in Missiles and UAVs;2020
5. Interdependent Estimation and Guidance With Zero-Effort-Miss Enforcement;IEEE Transactions on Aerospace and Electronic Systems;2019-08
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