Performance Analysis of Vector Tracking Algorithms for Weak GPS Signals in High Dynamics

被引:151
作者
Lashley, Matthew [1 ]
Bevly, David M. [2 ]
Hung, John Y. [1 ]
机构
[1] Auburn Univ, Dept Elect & Comp Engn, Auburn, AL 36849 USA
[2] Auburn Univ, Dept Mech Engn, Auburn, AL 36849 USA
关键词
Delay lock loop; frequency lock loop; Global Positioning System (GPS); Kalman filter; vector tracking;
D O I
10.1109/JSTSP.2009.2023341
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
This paper explores the ability of vector tracking algorithms to track weak Global Positioning System (GPS) signals in high dynamic environments. Traditional GPS receivers use tracking loops to track the GPS signals. The signals from each satellite are processed independently. In contrast, vector-based methods do not use tracking loops. Instead, all the satellite signals are tracked by a lone Kalman filter. The Kalman filter combines the tasks of signal tracking and navigation into a single algorithm. Vector-based methods can perform better than traditional methods in environments with high dynamics and low signal power. A performance analysis of the vector tracking algorithms is included. The ability of the algorithms to operate as a function of carrier to noise power density ratio, user dynamics, and number of satellites being used is explored. The vector tracking methods are demonstrated using data from a high fidelity GPS simulator. The simulation results show the vector tracking algorithms operating at a carrier to noise power density ratio of 19 dB-Hz through 2 G, 4 G, and 8 G coordinated turns. The vector tracking algorithms are also shown operating through 2 G and 4 G turns at a carrier to noise power density ratio of 16 dB-Hz.
引用
收藏
页码:661 / 673
页数:13
相关论文
共 27 条
  • [1] Abbott A.S., 2003, US Patent, Patent No. 6516021
  • [2] Bar-Shalom T. K. Y., 2001, Estimation with Applications to Tracking and Navigation
  • [3] Benson D., 2007, 63 ANN M ION, P749
  • [4] Brown R.G., 1996, INTRO RANDOM SIGNALS, DOI DOI 10.1002/RNC.4590020307
  • [5] Bullock J. B., 2006, MOB COMMUN INT, P459
  • [6] KALMAN FILTER BASED TRACKING SCHEME WITH INPUT ESTIMATION
    CHAN, YT
    HU, AGC
    PLANT, JB
    [J]. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 1979, 15 (02) : 237 - 244
  • [7] Copps E. M., 1980, Navigation. Journal of the Institute of Navigation, V27, P171
  • [8] CRANE RN, 2007, P NAT TECH M I NAV S
  • [9] Dierendonck A. J. V., 1996, PROGR ASTRONAUTICS A, V163
  • [10] Groves P. D, 2005, P 18 INT TECHN M SAT, P643