DocumentCode :
3604105
Title :
Unscented Attitude Estimator Based on Dual Attitude Representations
Author :
Kailong Li ; Lubin Chang ; Baiqing Hu
Author_Institution :
Dept. of Navig. Eng., Naval Univ. of Eng., Wuhan, China
Volume :
64
Issue :
12
fYear :
2015
Firstpage :
3564
Lastpage :
3576
Abstract :
This paper investigates an unscented attitude estimator based on modified Rodriguez parameter (MRP) and quaternion using a linearized attitude representation transformation. When the singularity transformation conditions do not occur, the developed filter can benefit from the MRP representation in terms of decreased calculation burden and improved filter consistency. When the singularity transformation conditions occur, the developed filter has a comparable performance in terms of accuracy to the well-known unscented quaternion estimator but with better filtering consistency and lower calculation burden. The validation of the developed filter is demonstrated through a high-precision strapdown inertial navigation system/Global Positioning System (SINS/GPS) simulation test and a low-cost SINS/GPS car-mounted experiment.
Keywords :
Kalman filters; inertial navigation; nonlinear filters; GPS; MRP; SINS; dual attitude representations; global positioning system; high-precision strapdown inertial navigation system; linearized attitude representation transformation; modified Rodriguez parameter; singularity transformation conditions; unscented attitude estimator; Covariance matrices; Estimation; Global Positioning System; Inertial navigation; Kalman filters; Quaternions; Attitude estimation; Kalman filter (KF); attitude representation; kalman filter (KF); linearized; strapdown inertial navigation system/Global Positioning System (SINS/GPS); strapdown inertial navigation system/Global Positioning System (SINS/GPS).;
fLanguage :
English
Journal_Title :
Instrumentation and Measurement, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9456
Type :
jour
DOI :
10.1109/TIM.2015.2454631
Filename :
7173046
Link To Document :
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