Journal of Projectiles, Rockets, Missiles and Guidance >
INS/GNSS Tight Integration Based on INS-aided FLL
Received date: 2013-05-21
Online published: 2025-05-30
In order to improve GNSS jamming immunity for low-cost guided weapon under complex electromagnetic environment, an INS/ GNSS tight coupling (TC) based on the INS-aided second order FLL was proposed. The Doppler frequency from the output of TC based on EKF and the loop filter of the second order FLL was used to control local carrier and code signal NCO, so the high dynamic performance was improved. A model of INS/GNSS tight integration filter was presented and the implementation of INS-aided tracking was given out. Dynamic simulation test shows that the TC based on INS-aided FLL can track carrier-to-noise 18 dB-Hz GPS L1 C/A signal, and the J/S level is 9 dB higher than that of stand-alone receiver.
Key words: INS/GNSS tight integration; INS-aided FLL; high dynamic tracking; anti-jamming; NCO
LI Chuanjun , PENG Zhongfeng , LI Xingcheng . INS/GNSS Tight Integration Based on INS-aided FLL[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2014 , 34(2) : 1 -5 . DOI: 10.15892/j.cnki.djzdxb.2014.02.009
| [1] | Razavi A, Gebre-Egziabher D, Akos D M. Carrier loop architectures for tracking weak GPS signals[J]. IEEE Transactions on Aerospace and Electronic Systems, 2008. 44(2): 697-710. |
| [2] | 于洁, 王新龙. SINS 辅助 GPS 跟踪环路超紧耦合系统设计[J]. 北京航空航天大学学报, 2010, 36(5): 606-609. |
| [3] | 赵琳, 赵洪斌, 闫超. 复杂环境下INS 辅助 GPS 跟踪环路研究[J]. 传感器与微系统, 2011, 30(10): 22– 25. |
| [4] | Angrisano A. GNSS/INS integration methods[D]. Naples,Italy: University of Naples, 2010. |
| [5] | 李传军. INS 辅助高动态卫星导航接收机关键技术研究[D]. 北京: 北京理工大学, 2013. |
| [6] | Guojiang Gao. INS-assisted high sensitivity GPS receivers for degraded signal navigation[D]. Calgary, Canada: University of Calgary, 2007. |
| [7] | ED Kaplan. Understanding GPS: Principles and applications[M]. London: Artech House, 1996. |
| [8] | Curran JT, Lachapelle G, Murphy CC. Improving the design of frequency lock loops for GNSS receivers[J]. Aero-space and Electronic Systems, IEEE Transactions on, 2012, 48(1): 850-868. |
| [9] | Ohlmeyer E J. Analysis of an ultratightly coupled GPS/INS system in jamming[C]// IEEE/ION, Position, Location, and Navigation Symposium, 2006: 44-53. |
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