Attitude estimation of nano-satellite according to navigation sensors using of combination method

被引：0
|
作者：
Toloei, A. [1 ]
Abbaszadehtoori, M. [1 ]
Shayan, M. [1 ]
机构：
[1] Department of Aerospace Engineering, Shahid Beheshti University, Tehran, Iran
来源：
International Journal of Engineering, Transactions A: Basics | 2015年 / 28卷 / 07期
关键词：
Attitude estimation - Attitude sensors - Combination method - Developed extended estimation quaternion - Measurement data - Navigation sensors - Quaternion estimations - Sun sensor;
D O I：
10.5829/idosi.ije.2015.28.07a.00
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1000 / 1015
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