Open Loop System Identification for a Quadrotor Helicopter System

被引：0
|
作者：
Schreurs, R. J. A. [1 ]
Weiland, S. [1 ]
Tao, H. [2 ]
Zhang, Q. [2 ]
Zhu, J. [2 ]
Zhu, Y. [2 ]
Xu, C. [2 ]
机构：
[1] Eindhoven Univ Technol, Dept Control Syst, Fac Elect Engn, NL-5612 AZ Eindhoven, Netherlands
[2] Zhejiang Univ, Inst Cyber Syst & Control, Dept Control Engn, Hangzhou 310027, Peoples R China
来源：
2013 10TH IEEE INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA) | 2013年
关键词：
SLIDING MODE CONTROL;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
This paper explains how the method of system identification can be applied to a quadrotor helicopter. First the first principles model is studied. The open-loop model is an unstable system, which is simulated using a closed-loop scheme. Then, a 12th order Auto Regressive Moving Average with eXogenous inputs (ARMAX) model is obtained based on the simulation data.
引用
收藏
页码：1702 / 1707
页数：6
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