DocumentCode :
1795166
Title :
A sliding-window least-squares estimation method for the biased velocity observation in the inertial-based integrated navigation systems
Author :
Jie Yang ; Wei Tan
Author_Institution :
Xi´an Satellite Control Center, State Key Lab. of Astronaut. Dynamics, Xi´an, China
fYear :
2014
fDate :
8-10 Aug. 2014
Firstpage :
1558
Lastpage :
1562
Abstract :
An effective estimation method is proposed for the constant horizontal velocity biases in the inertial-based integrated navigation systems. First, the analytical effects of the constant horizontal velocity biases on the exact inertial navigation errors are analyzed by the output-correction Kalman filter. Second, the sliding-window least-squares estimation method for the biased horizontal velocity observation is proposed where the INS error characteristic of horizontal velocities is sufficiently utilized. The simulation results illustrate that the estimation errors of constant horizontal velocity biases, which is derived within one Shuler oscillating period, are less than 5%. This estimation accuracy can be adequate in the inertial-based integrated navigation systems.
Keywords :
Kalman filters; aerospace control; inertial navigation; inertial systems; least squares approximations; velocity control; INS error characteristic; Shuler oscillating period; biased horizontal velocity observation; constant horizontal velocity biases; inertial navigation errors; inertial-based integrated navigation systems; output-correction Kalman filter; sliding-window least-squares estimation method; Accuracy; Equations; Estimation; Inertial navigation; Kalman filters; Mathematical model; Kalman filter; biased velocity observation; inertial navigation; integrated systems; output-correction;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Guidance, Navigation and Control Conference (CGNCC), 2014 IEEE Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4799-4700-3
Type :
conf
DOI :
10.1109/CGNCC.2014.7007424
Filename :
7007424
Link To Document :
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