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Non-linear robust filter design for satellite attitude determination

✍ Scribed by Xiong, K.; Liu, L.; Liu, Y.


Book ID
114442718
Publisher
The Institution of Engineering and Technology
Year
2010
Tongue
English
Weight
374 KB
Volume
4
Category
Article
ISSN
1751-8644

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## Abstract A problem of optimal estimation of a rotating vehicle's attitude with both differential equations of motion and observations of stars by onboard equipment is considered. The problem is formulated like a determinate non‐linear Kalman filter problem in quaternion terms. An exact analytica