Sub-Centimeter Precision Orbit Determination with GPS for Ocean Altimetry

被引:61
作者
Bertiger, Willy [1 ]
Desai, Shailen D. [1 ]
Dorsey, Angie [1 ]
Haines, Bruce J. [1 ]
Harvey, Nate [1 ]
Kuang, Da [1 ]
Sibthorpe, Ant [1 ]
Weiss, Jan P. [1 ]
机构
[1] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
基金
美国国家航空航天局;
关键词
Precision orbit determination; GPS; satellite altimetry; Jason; OSTM; ambiguity resolution; TOPEX/POSEIDON; SATELLITES; TRACKING; SERVICE; MODEL;
D O I
10.1080/01490419.2010.487800
中图分类号
P3 [地球物理学]; P59 [地球化学];
学科分类号
070403 [天体物理学]; 070902 [地球化学];
摘要
We assess the accuracy of JPL's estimated OSTM/Jason-2 Global Positioning System (GPS)-determined orbits based on residuals to independent satellite laser ranging (SLR) data, compared with orbits produced by different software from different data (SLR/DORIS), Geophysical Data Record version C (GDR-C) orbits, and altimeter crossover tests. All of these tests are consistent with sub-cm radial accuracy: high elevation SLR residual standard deviation lies at 6.8 mm, RMS differences from GDR-C in the radial component typically fall below a cm, and altimeter crossovers from JPL orbits have a variance 89 mm(2) smaller than altimeter crossovers from GDR-C orbits. Although RMS differences between radial components of different orbit solutions typically lie below a cm, we observe systematic dependences on both time and geography. The improved precision and accuracy of JPL's OSTM/Jason-2 orbit solutions rely on a new algorithm for applying constraints to integer carrier phase ambiguities. This algorithm is sufficiently robust to improve solutions despite half-cycle carrier phase identification issues in OSTM/Jason-2's BlackJack receiver. Although Jason-1 receiver performance differs, our algorithm should extend to Jason-1 processing (during the time span of nominal GPS receiver operations).
引用
收藏
页码:363 / 378
页数:16
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