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
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
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页码:1000 / 1015
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