返回
Two-axis euler rotation determination
DOI:10.1016/j.amc.2005.08.012.png)
摘要
En 中文
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. (c) 2005 Elsevier Inc. All rights reserved.

