测绘学报 ›› 2015, Vol. 44 ›› Issue (8): 848-857.doi: 10.11947/j.AGCS.2015.20140350

• 大地测量学与导航 • 上一篇    下一篇

GPS/INS紧组合的INS辅助周跳探测与修复

韩厚增1,2, 王坚1,2, 李增科1,2   

  1. 1. 中国矿业大学国土环境与灾害监测国家测绘地理信息局重点实验室, 江苏 徐州 221116;
    2. 中国矿业大学环境与测绘学院, 江苏 徐州 221116
  • 收稿日期:2014-07-03 修回日期:2015-05-11 出版日期:2015-09-20 发布日期:2015-09-02
  • 作者简介:韩厚增(1989-),男,博士生,研究方向为高精度GNSS/INS组合定位理论。E-mail:hanhouzeng@cumt.edu.cn
  • 基金资助:
    国土资源部公益性行业科研专项(201411007-1);国土环境与灾害监测国家测绘地理信息局重点实验室开放基金(LEDM2014B08);江苏高校优势学科建设工程项目(SZBF2011-6-B35)

Inertial Aided Kinematic GPS Cycle Slip Detection and Correction for GPS/INS Tightly Coupled System

HAN Houzeng1,2, WANG Jian1,2, LI Zengke1,2   

  1. 1. NASG Key Laboratory for Land Environment and Disaster Monitoring, China University of Mining and Technology, Xuzhou 221116, China;
    2. School of Environment Science and Spatial Informatics, China University of Mining and Technology, Xuzhou 221116, China
  • Received:2014-07-03 Revised:2015-05-11 Online:2015-09-20 Published:2015-09-02
  • Supported by:
    The Ministry of Land and Resources of Public Welfare Scientific Research(No. 201411007-1);A Project Funded by the NASG Key Laboratory of Land Environment and Disaster Monitoring(No.LEDM2014B08);Priority Academic Program Development of Jiangsu Higher Education Institutions(No. SZBF2011-6-B35)

摘要: 建立了GPS/INS紧组合定位模型,改正惯性器件误差及电离层折射误差,对不同组合观测量的误差影响进行了分析,构造不同观测值组合,提出了基于惯性信息辅助的GPS周跳自适应探测方法,分析了INS定位误差对周跳探测的影响,给出了周跳探测误报率及修复成功率评价指标,提出了一种周跳检测阈值自适应确定方法。利用实测组合导航试验数据验证本文的算法,文中模拟了不同的单历元多周跳及信号失锁条件,结果表明,在GPS信号完全失锁20 s内,该方法能准确检测和修复所有周跳,中断时间的延长降低了周跳修复的成功率;GPS信号部分失锁时,在模拟的90 s中断时段内仍能修复所有周跳;模拟了170历元的5 s间隔密集周跳,周跳探测成功率为100%,正确修复率为99.41%。

关键词: 惯性辅助, 周跳, 探测与修复, GPS/INS, 紧组合

Abstract: In order to improve the navigation performance and robustness, a GPS/INS tightly coupled model has been developed, the INS related bias and ionospheric errors were compensated and corrected, the impact of combination observations on cycle slip detection was investigated, and four combinations with the characteristics of longer wavelength, smaller noise and lower ionosphere effect were determined, then an innovative inertial aided adaptive cycle slip detection and correction algorithm based on the selected combination observations was presented, and the impact of INS positioning errors on cycle slip detection has been investigated, the probability of false alarm and success rate of cycle slip correction were utilized to enhance the integrity of cycle slip detection and correction, a new threshold determination criterion was provided to achieve robust cycle slip detection and correction. At last, a field test was utilized to verify and evaluate the performance of the proposed algorithm, multi-cycle slips and GPS gap scenarios were simulated, the results show that the scheme works effectively as long as the complete GPS data outage period is less than 20 second, the performance degrades as the outage period becomes longer; while during the partial data outage durations, the proposed scheme can fix the cycle slips correctly for the simulated 90 second partial outage due to the improved positioning accuracy, a total of 170 dense cycle slips (1 slip per 5 epochs)were introduced, it shows that all introduced cycle slips are successfully detected and the true fixing rate reaches 99.41%.

Key words: inertial aided, cycle slip, detection and correction, GPS/INS, tight coupling

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