The accuracy with which the GEOS-C altitude may be estimated over long (7 day) and short (40 minute) orbital arcs is investigated. Over the long are excellent agreement was attained between a simulation of the orbit determination process and a covariance analysis. Both approaches yielded RMS altitude errors of about 1.5 meters over the Caribbean calibration area and approximately 7.5 meters overall. The geopotential was identified as the largest error source. For the short arc, the covariance analysis revealed that the propagated altitude error is linearly dependent upon station survey component errors which are also the largest source of altitude errors. An Appendix contains the mathematics of covariance analysis as applied to orbit determ...
The GEOS-C spacecraft is scheduled to carry onboard a radar altimeter for the purpose of measuring t...
The orbit accuracies needed to support the global crustal dynamics project and recent satellite alti...
A satellite-to-satellite tracking experiment is planned between ATS-F and GEOS-C with a range accura...
Accuracy studies of radar and optical tracking of GEOS-C for altimeter experimen
Precise location of GEOS-C satellite in short arc orbits for radar altimeter tes
Effective utilization of data from the GEOS-C satellite for geoidal mapping was explored. Particular...
This study investigated the accuracies of orbit determinations in the radial coordinate utilizing cu...
The nature and improvement in satellite orbit determination when precise altimetric height data are ...
The feasibility of employing satellite to satellite tracking in lieu of ground based tracking to sat...
Station coordinates are given for the C-band radar GEOS-C altimeter calibration sites at Bermuda, Me...
The absolute bias calibration for the GEOS-3 intensive mode altimeter was measured using two satelli...
Data from the GEOS-3 altimeter were analyzed, for both the intensive and global modes, to determine ...
The effects of tropospheric and ionospheric refraction errors are analyzed for the GEOS-C altimeter ...
A pulse-limited split-gate-tracking radar altimeter was flown on Skylab and will be used aboard GEOS...
The determination of very precise orbits and geodynamic parameters from laser tracking data requires...
The GEOS-C spacecraft is scheduled to carry onboard a radar altimeter for the purpose of measuring t...
The orbit accuracies needed to support the global crustal dynamics project and recent satellite alti...
A satellite-to-satellite tracking experiment is planned between ATS-F and GEOS-C with a range accura...
Accuracy studies of radar and optical tracking of GEOS-C for altimeter experimen
Precise location of GEOS-C satellite in short arc orbits for radar altimeter tes
Effective utilization of data from the GEOS-C satellite for geoidal mapping was explored. Particular...
This study investigated the accuracies of orbit determinations in the radial coordinate utilizing cu...
The nature and improvement in satellite orbit determination when precise altimetric height data are ...
The feasibility of employing satellite to satellite tracking in lieu of ground based tracking to sat...
Station coordinates are given for the C-band radar GEOS-C altimeter calibration sites at Bermuda, Me...
The absolute bias calibration for the GEOS-3 intensive mode altimeter was measured using two satelli...
Data from the GEOS-3 altimeter were analyzed, for both the intensive and global modes, to determine ...
The effects of tropospheric and ionospheric refraction errors are analyzed for the GEOS-C altimeter ...
A pulse-limited split-gate-tracking radar altimeter was flown on Skylab and will be used aboard GEOS...
The determination of very precise orbits and geodynamic parameters from laser tracking data requires...
The GEOS-C spacecraft is scheduled to carry onboard a radar altimeter for the purpose of measuring t...
The orbit accuracies needed to support the global crustal dynamics project and recent satellite alti...
A satellite-to-satellite tracking experiment is planned between ATS-F and GEOS-C with a range accura...