| タイトル | Lunar Reconnaissance Orbiter Orbit Determination Accuracy Analysis |
| 本文（外部サイト） | http://hdl.handle.net/2060/20140008962 |
| 著者（英） | Slojkowski, Steven E. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 2014-05-05 |
| 言語 | eng |
| 内容記述 | LRO definitive and predictive accuracy requirements were easily met in the nominal mission orbit, using the LP150Q lunar gravity model. center dot Accuracy of the LP150Q model is poorer in the extended mission elliptical orbit. center dot Later lunar gravity models, in particular GSFC-GRAIL-270, improve OD accuracy in the extended mission. center dot Implementation of a constrained plane when the orbit is within 45 degrees of the Earth-Moon line improves cross-track accuracy. center dot Prediction accuracy is still challenged during full-Sun periods due to coarse spacecraft area modeling - Implementation of a multi-plate area model with definitive attitude input can eliminate prediction violations. - The FDF is evaluating using analytic and predicted attitude modeling to improve full-Sun prediction accuracy. center dot Comparison of FDF ephemeris file to high-precision ephemeris files provides gross confirmation that overlap compares properly assess orbit accuracy. |
| NASA分類 | Astrodynamics |
| レポートNO | GSFC-E-DAA-TN14298 |
| 権利 | Copyright, Distribution under U.S. Government purpose rights |
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