DocumentCode
233654
Title
Improved ICCP algorithm and its application in gravity matching aided inertial navigation system
Author
Liu Meiqi ; Wang Bo ; Deng Zhihong ; Fu Mengyin
Author_Institution
Nat. Key Lab. of Intell. Control & Decision of Complex Syst., Beijing Inst. of Technol., Beijing, China
fYear
2014
fDate
28-30 July 2014
Firstpage
562
Lastpage
567
Abstract
Considering two disadvantages in traditional gravity matching aided inertial navigation system, low matching accuracy and error accumulation, we propose an improved gravity matching algorithm and aided method for inertial navigation system. Instead of using the sequence sampling, the single point sampling is applied to improve the structure of proposed algorithm, enhancing the matching speed and efficiency. In the aided navigation system method, we use combination of Sage-Husa adaptive filter and strong-tracked Kalman filter to make further optimal estimation of the matching trajectory. Simulation results show the effectiveness of the real-time ICCP algorithm and the combined filter algorithm. Comparing to the traditional methods, proposed method provides higher matching and navigation accuracy.
Keywords
Kalman filters; adaptive filters; gravity; inertial navigation; signal sampling; ICCP algorithm; Sage-Husa adaptive filter; gravity matching algorithm; inertial navigation system; iterated closest contour point algorithm; single point sampling; strong tracked Kalman filter; trajectory matching; Accuracy; Algorithm design and analysis; Filtering algorithms; Filtering theory; Gravity; Navigation; combined filter; gravity aided navigation; single-point sampling;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896685
Filename
6896685
Link To Document