UDE-Based Robust Optimal Autopilot Design for Gliding-Guided Projectiles Subjected to Coupling Input Magnitude and Rate Saturation
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-021-00399-3.pdf
Reference30 articles.
1. Lim S, Cho S, Lee E (2020) Guidance to control arrival angle and altitude for an unpowered aerial vehicle. Int J Aeronaut Space Sci 21:1078–1091
2. Kim I, Choi HL, Jeon IS (2021) Closed-form impact-angle-control guidance of nose-dive missiles for maximum terminal speed. Int J Aeronaut Space Sci. https://doi.org/10.1007/s42405-021-00361-3
3. Chi HS, Lee YI, Lee CH (2021) A practical optimal guidance scheme under impact angle and terminal acceleration constraints. Int J Aeronaut Space Sci. https://doi.org/10.1007/s42405-020-00339-7
4. Han T (2017) Robust autopilot design for STT missiles with multiple disturbances using twisting control. Aerosp Sci Technol 70:428–434
5. Chwa D (2015) Fuzzy adaptive disturbance observer-based robust adaptive control for skid-to-turn missiles. IEEE Trans Aerosp Electron Syst 51(1):468–478
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