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