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General Formulas of Rotation Vector Based Attitude Algorithm of SDINS
Author(s): 
Pages: 18-22
Year: Issue:  2
Journal: AEROSPACE CONTROL

Keyword:  捷联式惯性导航*旋转矢量姿态*四元数;
Abstract: 这里给出了任意陀螺子样数下等效旋转矢量捷联姿态算法的一般结果.利用本文给出的公式,多子样等效旋转矢量算法可以很方便的由计算机得到,无需进行擎琐的推导,本文的工作为捷联姿态算法的设计提供了方便性和灵活性.
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