Quadrotor aircraft attitude estimation and control based on Kalman filter

被引：7
|
作者：
Wang, Shao-Hua [1 ]
Yang, Ying [1 ]
机构：
[1] College of Engineering, Peking University, Beijing 100871, China
来源：
Kongzhi Lilun Yu Yingyong/Control Theory and Applications | 2013年 / 30卷 / 09期
关键词：
D O I：
10.7641/CTA.2013.12261
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1109 / 1115
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