DocumentCode
233747
Title
Research on inertial information aided GPS tracking loop in high dynamic environment
Author
Jin Lei ; Chen Shuai
Author_Institution
Sch. of Autom., Nanjing Univ. Of Sci. & Technol., Nanjing, China
fYear
2014
fDate
28-30 July 2014
Firstpage
728
Lastpage
732
Abstract
GPS signal will generate the doppler frequency offset and its higher derivative when the precision guided weapon, such as missile rocket and so on, are in flight. The common tracking loop cannot track the signal steady, so that the receiver is likely to lose lock the signal and even to lose the ability of positioning and navigation. In order to track the signal steady in high dynamic environment, a method of the inertial information aided GPS tracking loop is given. The method provides the dopplor frequency offset aid for the tracking loop with the predicted frequency. The experiment results show that the method can meet the dynamic requirement of 50g missile acceleration with respect to the satellite and overcome the dynamical stress effect markedly. GPS receiver has the better ability of tracking dynamically.
Keywords
Doppler shift; Global Positioning System; missiles; satellite tracking; signal processing; Doppler frequency offset; GPS receiver; GPS signal generation; dynamical stress effect; high dynamic environment; inertial information aided GPS tracking loop; missile acceleration; missile rocket; precision guided weapon; satellite; Dopplor frequency offset; High dynamic; Inertial information aided; Tracking loop;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2014 33rd Chinese
Conference_Location
Nanjing
Type
conf
DOI
10.1109/ChiCC.2014.6896716
Filename
6896716
Link To Document