DocumentCode :
3201686
Title :
Quaternion optimization based in-flight calibration approach for POS
Author :
Kang Taizhong ; Jiancheng, Fang ; Wang Wei
Author_Institution :
“Inertial Technol.” Key Lab., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
fYear :
2012
fDate :
11-13 July 2012
Firstpage :
28
Lastpage :
31
Abstract :
Position and Orientation System (POS) is a key technology which provides motion compensation information for imaging sensor in airborne remote sensing. But precision of POS is degraded by gyroscope bias excursion as time flows, in-flight calibration is the most convenient way to solve this problem to the users, but the existing methods are mostly based on kalman filter, the effect of them to estimate the bias error is unpractical as affected severely by GPS measurement error and model error. On the basis of quaternion optimization based in-flight alignment approach, a novel airborne POS in-flight calibration approach based on quaternion optimization is devised in this paper, which adds the factor of attitude error promulgation by gyroscope bias error into the algorithm and gyroscope bias error is recognized by parse analysis. Flight experiments demonstrate that with the proposed algorithm the gyroscope bias error can be recognized in acceptable precision.
Keywords :
Global Positioning System; Kalman filters; calibration; error analysis; gyroscopes; image sensors; motion compensation; optimisation; remote sensing; GPS measurement error; GPS model error; Kalman filter; airborne POS in-flight calibration approach; airborne remote sensing; attitude error promulgation; flight experiments; gyroscope bias error estimation; gyroscope bias excursion; imaging sensor; motion compensation information; parse analysis; position and orientation system; quaternion optimization approach; Calibration; Eigenvalues and eigenfunctions; Global Positioning System; Gyroscopes; Kalman filters; Optimization; Quaternions; Position and Orientation System (POS); airborne remote sensing; error promulgation; gyroscope bias error; in-flight calibration; quaternion constrained least square;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation and Control Technology (ISICT), 2012 8th IEEE International Symposium on
Conference_Location :
London
Print_ISBN :
978-1-4673-2615-5
Type :
conf
DOI :
10.1109/ISICT.2012.6291631
Filename :
6291631
Link To Document :
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