| タイトル | TOPEX/POSEIDON operational orbit determination results using global positioning satellites |
| 本文（外部サイト） | http://hdl.handle.net/2060/19940025163 |
| 著者（英） | Jee, J.; Drain, T.; Lagattuta, F.; Wolff, P.; Guinn, J.; Sierra, V. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1994-02-15 |
| 言語 | eng |
| 内容記述 | Results of operational orbit determination, performed as part of the TOPEX/POSEIDON (T/P) Global Positioning System (GPS) demonstration experiment, are presented in this article. Elements of this experiment include the GPS satellite constellation, the GPS demonstration receiver on board T/P, six ground GPS receivers, the GPS Data Handling Facility, and the GPS Data Processing Facility (GDPF). Carrier phase and P-code pseudorange measurements from up to 24 GPS satellites to the seven GPS receivers are processed simultaneously with the GDPF software MIRAGE to produce orbit solutions of T/P and the GPS satellites. Daily solutions yield subdecimeter radial accuracies compared to other GPS, LASER, and DORIS precision orbit solutions. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 94N29666 |
| 権利 | No Copyright |
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