DocumentCode :
711164
Title :
On the identifiability of noise statistics and adaptive KF design for robust GNSS carrier tracking
Author :
Vila-Valls, Jordi ; Closas, Pau ; Fernandez-Prades, Carles
Author_Institution :
Centre Tecnol. de Telecomunicacions de Catalunya, Barcelona, Spain
fYear :
2015
fDate :
7-14 March 2015
Firstpage :
1
Lastpage :
10
Abstract :
Carrier synchronization is of paramount importance in any communications or positioning system. Mass-market Global Navigation Satellite System (GNSS) receivers typically implement traditional carrier tracking techniques based on well-established phase-locked loop architectures, which are only reliable in quite benign propagation conditions. Under nonnominal harsh propagation conditions, the signal may be affected by shadowing, strong fading, multipath or severe ionospheric scintillation, and thus, traditional architectures are not valid anymore and there exists an actual need for robust tracking solutions. Several approaches to overcome the conventional PLL limitations have appeared during the last decade, being the Kalman filter (KF) based architectures the most promising research line. The main drawback of standard KFs is the assumption of perfectly known process and measurement noise statistics, a knowledge that is always constrained by the system model accuracy. Beyond heuristic solutions, a general framework for the design of adaptive KFs correctly dealing with both process and measurement noises, that would be of capital importance for the practitioner, has not been established. The main goal of this contribution is to provide a clear answer to this fundamental question. It is shown that the main driver on the KF performance is not the adjustment of the measurement noise but the adequate tuning of the process noise statistics. Within this framework, a comprehensive discussion is given for the correct design of adaptive KF architectures for robust carrier tracking applications, where the key idea is to use two independent noise statistics estimation strategies to sequentially adapt both parameters. The design choice is supported by a discussion on the identifiability of the noise statistics´ parameters. Simulation results are provided showing the need of fully adaptive solutions, and the achieved performance gain of KF-based architectures when compared to tra- itional tracking loops.
Keywords :
Global Positioning System; adaptive Kalman filters; measurement errors; measurement uncertainty; phase locked loops; Kalman filter based architectures; PLL; adaptive KF design; carrier synchronization; fading; identifiability; ionospheric scintillation; mass-market global navigation satellite system receivers; measurement noise statistics; multipath; nonnominal harsh propagation conditions; performance gain; phase-locked loop architectures; positioning system; process noise statistics; research line; robust GNSS carrier tracking; shadowing; tracking loops; Estimation; Joints; Mathematical model; Noise; Noise measurement; Phase locked loops; Standards;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2015 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5379-0
Type :
conf
DOI :
10.1109/AERO.2015.7118929
Filename :
7118929
Link To Document :
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