论文标题
GIPSYX/RTGX,一种用于空间大地测量操作和研究的新工具
GipsyX/RTGx, A New Tool Set for Space Geodetic Operations and Research
论文作者
论文摘要
GIPSYX/RTGX是使用三种测量技术的测量值:全球导航卫星系统(GNSS),卫星激光范围(SLR)和多普勒甲型术和放射线(Doppler Orbitography and radiopsienting(由Satellite)组成的(dories contected),GIPSYX/RTGX是用于定位,导航,定时和地球科学的下一代下一代软件包。正在开发的基线干涉法(VLBI)非常长。该软件促进了在后处理和实时进行的真实或模拟数据上使用Kalman滤波器方法对大地测量和地球物理参数进行综合估计。估计的参数包括站坐标和速度,卫星轨道和时钟,地球取向,电离层和对流层延迟。该软件还能够通过分析和时间序列的地面站坐标来充分实现动态陆地参考。 我们介绍了其新体系结构的一些关键方面,并描述了其一些主要应用程序,包括美国空军下一代GPS下一代GPS运营控制领域(OCX)的实时轨道确定和阵地预测,以及JPL的全球差异GPS(GDGPS)系统中,支持用户范围误差(URE),为$ <$ 5 cm rms $ <$ 5 cm rms;精密后处理GNSS轨道确定,包括JPL在2 cm RMS范围内对国际GNSS服务(IGS)的贡献;对于静态和运动学上的歧义分辨率的精确点定位(PPP),用于2 mm水平的地球应用,静态定位为6.5 mm垂直可重复性;低地球轨道(LEO)卫星的操作轨道和时钟确定,例如NASA的重力恢复和气候实验(GRACE)任务(GRACE)任务,宽限期相对时钟在20 ps级别。
GipsyX/RTGx is the Jet Propulsion Laboratory's (JPL) next generation software package for positioning, navigation, timing, and Earth science using measurements from three geodetic techniques: Global Navigation Satellite Systems (GNSS), Satellite Laser Ranging (SLR), and Doppler Orbitography and Radiopositioning Integrated by Satellite (DORIS); with Very Long Baseline Interferometry (VLBI) under development. The software facilitates combined estimation of geodetic and geophysical parameters using a Kalman filter approach on real or simulated data in both post-processing and in real-time. The estimated parameters include station coordinates and velocities, satellite orbits and clocks, Earth orientation, ionospheric and tropospheric delays. The software is also capable of full realization of a dynamic terrestrial reference through analysis and combination of time series of ground station coordinates. We present some key aspects of its new architecture, and describe some of its major applications, including Real-time orbit determination and ephemeris predictions in the U.S. Air Force Next Generation GPS Operational Control Segment (OCX), as well as in JPL's Global Differential GPS (GDGPS) System, supporting User Range Error (URE) of $<$ 5 cm RMS; precision post-processing GNSS orbit determination, including JPL's contributions to the International GNSS Service (IGS) with URE in the 2 cm RMS range; Precise point positioning (PPP) with ambiguity resolution, both statically and kinematically, for geodetic applications with 2 mm horizontal, and 6.5 mm vertical repeatability for static positioning; Operational orbit and clock determination for Low Earth Orbiting (LEO) satellites, such as NASA's Gravity Recovery and Climate Experiment (GRACE) mission with GRACE relative clock alignment at the 20 ps level.