DocumentCode :
716026
Title :
Improvement in tracking loop threshold of high dynamic GNSS receiver by installation of crystal oscillator on gyroscopic mounting
Author :
Abedi, Maryam ; Tian Jin
Author_Institution :
Sch. of Electron. & Inf., Beihang Univ., Beijing, China
fYear :
2015
fDate :
12-16 April 2015
Firstpage :
522
Lastpage :
527
Abstract :
In high dynamic GNSS receivers, replica carrier is polluted by dynamic loads which modulated on it and generate clock drift as frequency and phase error. These dynamic loads consist of steady state acceleration, sinusoidal vibration, mechanical and acoustic random vibrations. As steady state load exists all over the trajectory and causes great phase deviation, therefor phase lock is lost and the sensitive phase lock detector distinguishes it and transits back to FLL, therefore the dominant tracking loop in high dynamic receivers is FLL. According to the calculations, all dynamic loads cause some amount of frequency deviation (feo) or jitter(3σvFLL), it is also worth remembering that among them random vibration causes great frequency jitter and impacts FLL significantly.
Keywords :
crystal oscillators; gyroscopes; jitter; satellite navigation; vibrations; acoustic random vibrations; crystal oscillator installation; dynamic loads; frequency deviation; frequency jitter; gyroscopic mounting; high dynamic GNSS receiver; mechanical random vibrations; replica carrier; sinusoidal vibration; steady state acceleration; tracking loop threshold; Acoustics; Crystals; Global Positioning System; Receivers; Vehicle dynamics; Vehicles; Vibrations; Acoustic Pressure Load; FLL; GPS; Gyro; High Dynamic GNSS Receiver; Launch Vehicle; Mounting; PLL; Random Vibration; Sinusoidal Vibrations; Steady State Acceleration; Tracking Loop;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Frequency Control Symposium & the European Frequency and Time Forum (FCS), 2015 Joint Conference of the IEEE International
Conference_Location :
Denver, CO
Print_ISBN :
978-1-4799-8865-5
Type :
conf
DOI :
10.1109/FCS.2015.7138898
Filename :
7138898
Link To Document :
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