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Three-dimensional tracking of a lunar satellite with differential Very-Long-Baseline-Interferometry
Institution:1. College of Civil Engineering, Taiyuan University of Technology, Taiyuan 030024, China;2. Department of Computer Science, University of Freiburg, Freiburg 79110, Germany;1. Institute for Communications and Navigation of the German Aerospace Center (DLR), Oberpfaffenhofen, 822354 Wessling, Germany;2. Department of Teleinformatics Engineering, Federal University of Ceara (UFC), CP 6007, Fortaleza, Ceara 60455-970, Brazil;3. Institute for Circuit Theory and Signal Processing, Munich University of Technology (TUM), 80290 Munich, Germany;1. College of Information Engineering, Shenzhen University, Shenzhen, PR China;2. Department of Electrical and Computer Engineering, McMaster University, Hamilton, Canada;3. Department of Electronic Engineering, City University of Hong Kong, Hong Kong
Abstract:Lunar gravimetry mission in the Japanese lunar exploration project SELENE (Selenological and Engineering Explorer) is characterized by inter-satellite tracking by means of a relay satellite in a high eccentric orbit, combined with differential Very-Long-Baseline-Interferometry (ΔVLBI) and conventional 2-way Doppler tracking. ΔVLBI provides information on the satellite position and velocity complementary to conventional range and range rate measurement, and allows us to measure lunar gravitational accelerations in all the three components. In this article, ΔVLBI and 2-way Doppler numerical simulation results are compared to those obtained from 2-way Doppler observations only, so that we can evaluate the contribution of ΔVLBI to the SELENE lunar gravimetry mission.
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