Attitude error representations for Kalman filtering

被引:491
作者
Markley, FL [1 ]
机构
[1] NASA, Goddard Space Flight Ctr, Guidance Navigat & Control Syst Engn Branch, Greenbelt, MD 20771 USA
关键词
Estimation - Mathematical models - Position measurement - Vectors;
D O I
10.2514/2.5048
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The quaternion has the lowest dimensionality possible for a globally nonsingular attitude representation. The quaternion must obey a unit norm constraint, though,which has led to the development of an extended Kalman filter using a quaternion for the global attitude estimate and a three-component representation for attitude errors. Various attitude error representations are considered for this multiplicative extended Kalman filter, which incorporates a nonlinear, norm preserving quaternion reset operation. Second-order bias corrections are computed in this framework.
引用
收藏
页码:311 / 317
页数:7
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