@inproceedings{5e6cac3100e545bb89ab5d7467ae7d92,
title = "Strong adaptive attitude tracking controller design with dual-model structure for unmanned helicopter",
abstract = "The main objective of this research is to provide an efficient and flexible control approach for unmanned helicopter (UH) to overcome the major difficulties in aerodynamic parameter uncertainties. A strong adaptive tracking controller with dual-model structure, which has significant advantages of separating model tracking parameter design from adaptive control, is presented for the attitude control problem, and the system stability margin is improved in the process of adjustment parameter correction and tracking error is reduced. The sensors, noise influence on adjustable parameter correction has been reduced through adding a state filter behind the adjustable system. The efficiency and feasibility of this method are provided by flight test.",
keywords = "adaptive control, decoupling, flight test, unmanned helicopter",
author = "Shouzhao Sheng and Chenwu Sun and Haibin Duan and Fahad Farooq and Masood, \{Rana Javed\}",
note = "Publisher Copyright: {\textcopyright} 2014 TCCT, CAA.; Proceedings of the 33rd Chinese Control Conference, CCC 2014 ; Conference date: 28-07-2014 Through 30-07-2014",
year = "2014",
month = sep,
day = "11",
doi = "10.1109/ChiCC.2014.6896615",
language = "英语",
series = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",
publisher = "IEEE Computer Society",
pages = "162--167",
editor = "Shengyuan Xu and Qianchuan Zhao",
booktitle = "Proceedings of the 33rd Chinese Control Conference, CCC 2014",
address = "美国",
}