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月内部構造の制約科学目標の達成見込みに関する検討

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Sgr A*/éæ²³ç³»ä¸å¿ VLBAç ç©¶ï½ãµãããªæ³¢VLBIã¸ ï¼æ¥æ¬ã®è²¢ç® ... - VERA

M. Sato, 2010, PASJ, 62, pp.287, Distance to G14.33ï¼0.64 ... - VERA

Hirota T. et al. 2007, PASJ, 59, 897, Distance to Orion KL ... - VERA

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Result of numerical simulationk2 uncertainty vs arc length1%Orbit: 100km x 800km, Inclination: 90 deg, Lander coordinates (0 deg, 0 deg),Ground stations operated 6 hours/day, Mission duration: 3 months1% of k2 accuracy can be achieved by SELENE-2 VLBI mission.

月内部構造の制約科学目標の達成見込みに関する検討

Page 1: 月着陸探査計画 SELENE-
Page 8 and 9: How sensitive are the geodeticmeasu
Page 10 and 11: Total likelihood functionただし
Page 12 and 13: 12開発課題と開発状
Page 14 and 15: アルミナ基板のパッチ
Page 16: Conclusions• 次期月着陸

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æçé¸æ¢æ»è¨ç»SELENE-2ã«ããã VLBIæè¡ãç¨ããæéå ... - VERA