Persistent Identifier
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hdl:2014/44055 |
Publication Date
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2013-02-11 |
Title
| The role of GRAIL orbit determination in preprocessing of gravity science measurements |
Author
| Kruizing, Gerharda (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Asmar, Sami (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Fahnestock, Eugene (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Harvey, Nate (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Kahan, Daniel (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Konopliv, Alex (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Oudrhiri, Kamal (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Paik, Meegyeong (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Park, Ryan (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Strekalov, Dmitry (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Watkins, Michael (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013)
Yuan, Dah-Ning (Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013) |
Point of Contact
|
Use email button above to contact.
Kruizing, Gerharda |
Description
| The Gravity Recovery And Interior Laboratory (GRAIL) mission has constructed a lunar gravity field with unprecedented uniform accuracy on the farside and nearside of the Moon. GRAIL lunar gravity field determination begins with preprocessing of the gravity science measurements by applying corrections for time tag error, general relativity, measurement noise and biases. Gravity field determination requires the generation of spacecraft ephemerides of an accuracy not attainable with the pre-GRAIL lunar gravity fields. Therefore, a bootstrapping strategy was developed, iterating between science data preprocessing and lunar gravity field estimation in order to construct sufficiently accurate orbit ephemerides.This paper describes the GRAIL measurements, their dependence on the spacecraft ephemerides and the role of orbit determination in the bootstrapping strategy. Simulation results will be presented that validate the bootstrapping strategy followed by bootstrapping results for flight data, which have led to the latest GRAIL lunar gravity fields. |
Subject
| Other |
Production Date
| 2013-02-11 |