Two-axis euler rotation determination
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摘要
Satellite orientation is usually expressed in terms of euler rotations about the three principal axes. Usually, the orientation is determined using the measurements of at least two known vectors. A variant to this problem is considered in this note.
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论文评审过程:Available online 26 September 2005.
论文官网地址:https://doi.org/10.1016/j.amc.2005.08.012