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 :
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