Output feedback control of hypersonic vehicles based on neural network and high gain observer
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Computer Science
Link
http://link.springer.com/content/pdf/10.1007/s11432-011-4194-y.pdf
Reference19 articles.
1. Wang Q, Stengel R F. Robust nonlinear control of a hypersonic aircraft. AIAA J Guid Control Dyn, 2000, 23: 577–585
2. Xu H J, Mirmirani M D, Ioannou P A. Adaptive sliding mode control design for a hypersonic flight Vehicle. AIAA J Guid Control Dyn, 2004, 27: 829–838
3. Groves K P, Sithorsson D O, Serrani A, et al. Reference command tracking for a linearized model of an air-breathing hypersonic vehicle. In: Proc of the 2005 AIAA Guidance, Navigation, and Control Conference and Exhibit. San Francisco, California, USA, 2005. AIAA 2005-6144
4. Kuipers M, Ioannou P. Robust adaptive multiple model controller design for an airbreathing hypersonic vehicle model. In: Proc of the 2008 AIAA Guidance, Navigation and Control Conference and Exhibit. Honolulu, Hawaii, USA, 2008. AIAA 2008-7142
5. Wilcox Z D, MacKunis W, Bhat S, et al. Robust nonlinear control of a hypersonic aircraft in the presence of aerothermoelastic effects. In: Proc of the 2009 American Control Conference. St. Louis, MO, USA, 2009. 2533–2538
Cited by 25 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. Aircraft Middle and Final Stage Attitude Control on Fully Actuated System Theory;2024 3rd Conference on Fully Actuated System Theory and Applications (FASTA);2024-05-10
2. Output feedback control for hypersonic flight vehicles via distributed high-gain observer;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2024-05-02
3. Adaptive Robust Tracking Control for Near Space Vehicles with Multi-Source Disturbances and Input–Output Constraints;Actuators;2022-09-23
4. Deriving a Control-Oriented Model for an Axisymmetric Vehicle With the Power-Law Revolution Nose;Journal of Aerospace Technology and Management;2020-09-16
5. Robust output feedback control of fixed-wing aircraft;Aircraft Engineering and Aerospace Technology;2020-07-23
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