ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS
| dc.contributor.author | Jinglai, Shen | |
| dc.contributor.author | Jinyuan, Gao | |
| dc.date.accessioned | 2024-08-27T20:38:48Z | |
| dc.date.available | 2024-08-27T20:38:48Z | |
| dc.date.issued | 1998-10-25 | |
| dc.description.abstract | The design of a maneuverable flight command tracking system using nonlinear dynamic inversion is briefly introduced at first. And then a robust controller to improve the robustness of dynamic inversion is designed using the method of μ analysis and synthesis. The detailed design process and results are presented. Simulations show that the robust dynamic inversion controller yields good results. | |
| dc.description.uri | https://hkxb.buaa.edu.cn/CN/abstract/abstract11488.shtml | |
| dc.format.extent | 5 pages | |
| dc.genre | journal articles | |
| dc.identifier | doi:10.13016/m21wnt-vswz | |
| dc.identifier.citation | Jinglai, Shen, and Gao Jinyuan. “ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS” 19, no. 5 (October 25, 1998): 592–96. https://hkxb.buaa.edu.cn/CN/abstract/abstract11488.shtml | |
| dc.identifier.uri | http://hdl.handle.net/11603/35917 | |
| dc.language.iso | en_US | |
| dc.publisher | Beijing University of Aeronautics & Astronautics | |
| dc.relation.isAvailableAt | The University of Maryland, Baltimore County (UMBC) | |
| dc.relation.ispartof | UMBC Mathematics and Statistics Department | |
| dc.rights | This item is likely protected under Title 17 of the U.S. Copyright Law. Unless on a Creative Commons license, for uses protected by Copyright Law, contact the copyright holder or the author. | |
| dc.title | ROBUST DYNAMIC INVERSION DESIGN OF MANEUVERABLE FLIGHT COMMAND TRACKING SYSTEMS | |
| dc.type | Text | |
| dcterms.creator | https://orcid.org/0000-0003-2172-4182 |