Robust vertical takeoff and landing aircraft control via integral sliding mode
| dc.citation.epage | 388 | en_US |
| dc.citation.issue | 4 | en_US |
| dc.citation.spage | 383 | en_US |
| dc.citation.volume | 150 | en_US |
| dc.citation.woscount | 18 | |
| dc.contributor.author | Huang, YJ | en_US |
| dc.contributor.author | Kuo, TC | en_US |
| dc.contributor.author | Way, HK | en_US |
| dc.contributor.department | 電信工程研究所 | zh_TW |
| dc.contributor.department | Institute of Communications Engineering | en_US |
| dc.date.accessioned | 2014-12-08T15:40:41Z | |
| dc.date.available | 2014-12-08T15:40:41Z | |
| dc.date.issued | 2003-07-01 | en_US |
| dc.description.abstract | Reduced equivalent systems have inherent closed-loop poles at the origin in the sliding mode for conventional sliding mode control (SMC). A systematic design strategy is developed for arbitrarily placing all SMC closed-loop poles. The speed control of a vertical takeoff and landing aircraft whose aerodynamic parameters vary considerably during flight is investigated. An outstanding output tracking performance and robustness against system parameter uncertainties and external disturbances are achieved. | en_US |
| dc.identifier.doi | 10.1049/ip-cta:20030593 | en_US |
| dc.identifier.issn | 1350-2379 | en_US |
| dc.identifier.journal | IEE PROCEEDINGS-CONTROL THEORY AND APPLICATIONS | en_US |
| dc.identifier.uri | http://dx.doi.org/10.1049/ip-cta:20030593 | en_US |
| dc.identifier.uri | https://ir.lib.nycu.edu.tw/handle/11536/27755 | |
| dc.identifier.wosnumber | WOS:000185484600008 | |
| dc.language.iso | en_US | en_US |
| dc.title | Robust vertical takeoff and landing aircraft control via integral sliding mode | en_US |
| dc.type | Article | en_US |