@inproceedings{4c8cecb4797f4332a85dabd8b3cfb538,
title = "Missile attitude control in a large flight envelope based on the linear active disturbance rejection control approach",
abstract = "Usually the missile attitude control process in a large flight envelope has strong time-varying and nonlinear characteristics, so the controller parameter is difficultly scheduled with conventional PID control approach. In this study a linear active disturbance rejection control approach based on reduced-order linear extended state observer is proposed. The approach is employed to the attitude controller for a supersonic missile in attack with high angle. It is not hard to determine the proposed controller parameter, and the numeral simulations show that the presented approach has a very good capability on tracking attitude command.",
keywords = "attitude control, large flight envelope, linear active disturbance rejection control, reduced-order linear extended state observer",
author = "Hui Li and Yu Fan and Fengyi Li and Chuang Song and Zhide Yin",
note = "Publisher Copyright: {\textcopyright} 2014 IEEE.; 6th IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014 ; Conference date: 08-08-2014 Through 10-08-2014",
year = "2015",
month = jan,
day = "12",
doi = "10.1109/CGNCC.2014.7007376",
language = "English",
series = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "1219--1223",
booktitle = "2014 IEEE Chinese Guidance, Navigation and Control Conference, CGNCC 2014",
address = "United States",
}