Kim Younsil, Song Junesol, Kee Changdon, Park Byungwoon
Institute of Advanced Aerospace Technology, School of Mechanical and Aerospace Engineering, Seoul National University, 1 Gwanak-ro, Gwanak-gu, Seoul 151-744, Korea.
School of Mechanical and Aerospace Engineering, Sejong University, 209 Neungdong-ro, Gwangjin-gu, Seoul 143-747, Korea.
Sensors (Basel). 2015 Sep 30;15(10):25336-65. doi: 10.3390/s151025336.
This paper presents a means of carrier phase cycle slip detection for an inertial-aided global positioning system (GPS), which is based on consideration of the satellite geometry. An integrated navigation solution incorporating a tightly coupled time differenced carrier phase (TDCP) and inertial navigation system (INS) is used to detect cycle slips. Cycle-slips are detected by comparing the satellite-difference (SD) and time-difference (TD) carrier phase measurements obtained from the GPS satellites with the range estimated by the integrated navigation solution. Additionally the satellite geometry information effectively improves the range estimation performance without a hardware upgrade. And the covariance obtained from the TDCP/INS filter is used to compute the threshold for determining cycle slip occurrence. A simulation and the results of a vehicle-based experiment verify the cycle slip detection performance of the proposed algorithm.
本文提出了一种用于惯性辅助全球定位系统(GPS)的载波相位周跳检测方法,该方法基于对卫星几何结构的考虑。采用一种结合了紧密耦合时间差分载波相位(TDCP)和惯性导航系统(INS)的组合导航解决方案来检测周跳。通过将从GPS卫星获得的星间差分(SD)和时间差分(TD)载波相位测量值与组合导航解决方案估计的距离进行比较来检测周跳。此外,卫星几何信息在无需硬件升级的情况下有效提高了距离估计性能。并且利用从TDCP/INS滤波器获得的协方差来计算用于确定周跳发生的阈值。仿真和基于车辆的实验结果验证了所提算法的周跳检测性能。