Dynamic output feedback H∞ attitude control for hypersonic gliding vehicles
Saved in:
| Title: | Dynamic output feedback H∞ attitude control for hypersonic gliding vehicles |
|---|---|
| Authors: | Zhang, Weidong, Huang, Xianlin, Gao, Xiao Zhi |
| Source: | INTERNATIONAL JOURNAL OF INNOVATIVE COMPUTING INFORMATION AND CONTROL. 13(4):1351-1368 |
| Publisher Information: | 2017. |
| Publication Year: | 2017 |
| Subject Terms: | Hypersonic gliding vehicle, ta214, ta213, Parallel distributed compensation (PDC), Dynamic output feedback controller, Linear matrix inequality (LMI), T-S fuzzy model, H performance |
| Document Type: | Article |
| Language: | English |
| ISSN: | 1349-4198 |
| Access URL: | http://juuli.fi/Record/0281330717 |
| Accession Number: | edsair.CSC...........864bd5658cc9fabeb1f0fcf57076403b |
| Database: | OpenAIRE |
Full Text Finder 
Nájsť tento článok vo Web of Science Be the first to leave a comment!