GPS precise tracking of TOPEX/POSEIDON: Results and implications

A reduced dynamic filtering strategy that exploits the unique geometric strength of the Global Positioning System(GPS) to minimize the effects of force model errors has yielded orbit solutions for TOPEX/POSEIDON which appear accurate to better than 3 cm (1 σ) in the radial component. Reduction of force model error also reduces the geographic correlation of the orbit error. With a traditional dynamic approach, GPS yields radial orbit accuracies of 4–5 cm, comparable to the accuracy delivered by satellite laser ranging and the Doppler orbitography and radio positioning integrated by satellite (DORIS) tracking system. A portion of the dynamic orbit error is in the Joint Gravity Model-2 (JGM-2); GPS data from TOPEX/POSEIDON can readily reveal that error and have been used to improve the gravity model.

[1]  Geoffrey Blewitt,et al.  An Automatic Editing Algorithm for GPS data , 1990 .

[2]  Jiun-Tsong Wu,et al.  Gravity field improvement using global positioning system data from TOPEX/Poseidon: A covariance analysis , 1992 .

[3]  G. Bierman Factorization methods for discrete sequential estimation , 1977 .

[4]  C. Valorge,et al.  Precise Centre National d'Etudes Spatiales orbits for TOPEX/POSEIDON: Is reaching 2 cm still a challenge? , 1994 .

[5]  T. P. Yunck,et al.  Non-dynamic decimeter tracking of earth satellites using the Global Positioning System , 1986 .

[6]  W. I. Bertiger,et al.  Minimizing selective availability error on satellite and ground global positioning system measurements , 1992 .

[7]  Yves Menard,et al.  Calibration of the TOPEX/POSEIDON altimeters at Lampedusa: Additional results at Harvest , 1994 .

[8]  E. J. Christensen,et al.  Observations of geographically correlated orbit errors for TOPEX/Poseidon using the global positioning system , 1994 .

[9]  John C. Ries,et al.  Absolute positioning using Doris tracking of the SPOT‐2 satellite , 1992 .

[10]  Thomas P. Yunck,et al.  Precise tracking of remote sensing satellites with the Global Positioning System , 1990 .

[11]  Bob E. Schutz,et al.  Precision orbit determination for TOPEX/POSEIDON , 1994 .

[12]  George Walton Rosborough Satellite orbit perturbations due to the geopotential , 1986 .

[13]  Michael B. Heflin,et al.  Absolute far-field displacements from the 28 June 1992 Landers earthquake sequence , 1993, Nature.

[14]  E. J. Christensen,et al.  Calibration of TOPEX/POSEIDON at Platform Harvest , 1994 .

[15]  Penina Axelrad,et al.  Calibration of the TOPEX altimeter using a GPS buoy , 1994 .

[16]  Sheng Yuan Zhu,et al.  GPS satellite-to-satellite tracking for TOPEX/Poseidon precise orbit determination and gravity field model improvement , 1995 .

[17]  Richard D. Ray,et al.  Oceanic tides from Geosat altimetry , 1990 .

[18]  James J. Spilker,et al.  GPS Signal Structure and Performance Characteristics , 1978 .

[19]  W. G. Melbourne,et al.  Scientific Applications of GPS on Low Earth Orbiters , 1994 .

[20]  Scott Mitchell,et al.  Geographically correlated orbit error for the Topex satellite using GPS tracking , 1990 .

[21]  H. Fliegel,et al.  Global Positioning System Radiation Force Model for geodetic applications , 1992 .

[22]  J. T. Wu,et al.  Minimizing selective availability error on Topex GPS measurements , 1990 .

[23]  W. I. Bertiger,et al.  Effects of antenna orientation on GPS carrier phase , 1992 .

[24]  Craig L. Purdy,et al.  Satellite/sensors for monitoring earth's oceans from space , 1995 .

[25]  Jiun-Tsong Wu,et al.  Gravity field improvement using GPS data from Topex/Poseidon - A covariance analysis , 1990 .

[26]  Bob E. Schutz,et al.  Gravity model development for TOPEX/POSEIDON: Joint gravity models 1 and 2 , 1994 .

[27]  Chet Koblinksky,et al.  GEOSAT vs. SEASAT , 1988 .

[28]  M. Kaplan Modern Spacecraft Dynamics and Control , 1976 .

[29]  Thomas P. Yunck,et al.  The GPS flight experiment on TOPEX/POSEIDON , 1994 .

[30]  Thomas P. Yunck,et al.  Reduced-dynamic technique for precise orbit determination of low earth satellites , 1991 .

[31]  Hyung-Jin Rim,et al.  Dynamic orbit determination using GPS measurements from TOPEX/POSEIDON , 1994 .

[32]  R. J. Milliken,et al.  PRINCIPLE OF OPERATION OF NAVSTAR AND SYSTEM CHARACTERISTICS (GPS SYSTEM DESCRIPTION) , 1978 .

[33]  E. W. Schwiderski,et al.  On charting global ocean tides , 1980 .

[34]  Pascal Willis,et al.  First assessment of GPS-based reduced dynamic orbit determination on TOPEX/Poseidon , 1994 .

[35]  E. J. Christensen,et al.  TOPEX/POSEIDON mission overview , 1994 .