@inproceedings{4c21ac15970b4fa9adad19d9b0341104,
title = "A flight controller based on extend state observer for quadrotor aerial vehicles",
abstract = "In order to solve the problems of parameter uncertainty and sensitivity to external disturb, a flight control system for quadrotor based on extend state observer was proposed. First, the flight dynamic model for quadrotor was built. Then, the effect resulted from parameter uncertainty and external disturb was taken as general system disturb so it could be estimated online by extend state observer. Further, the error feedback was designed to ensure the control system performance. Finally, simulations verify the controller.",
keywords = "extend state observer, flight control system, Quadrotor, robustness",
author = "Shangjing Wu and Ke Lu and Zhengzhong Wang and Zhenghua Liu",
note = "Publisher Copyright: {\textcopyright} 2017 Technical Committee on Control Theory, CAA.; 36th Chinese Control Conference, CCC 2017 ; Conference date: 26-07-2017 Through 28-07-2017",
year = "2017",
month = sep,
day = "7",
doi = "10.23919/ChiCC.2017.8027894",
language = "英语",
series = "Chinese Control Conference, CCC",
publisher = "IEEE Computer Society",
pages = "3469--3472",
editor = "Tao Liu and Qianchuan Zhao",
booktitle = "Proceedings of the 36th Chinese Control Conference, CCC 2017",
address = "美国",
}