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Summary of the orbit determination of NOZOMI spacecraft for all the mission period
Abstract Japanese first Mars explorer NOZOMI, which was launched in July 1998, suffered several problems during the operation period of more than five years. It could have reached near Mars at theExpand
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VLBI Observation of Spacecraft for Navigation –Approaches with Group Delay and Phase Delay –
Very long baseline interferometry (VLBI) has high sensitivity in coordinate measurement in the celestial sphere. Joint use of VLBI and range and range rate measurement can enhance the accuracy of theExpand
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Status report on VLBI application for space navigation of Hayabusa
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Acceleration Estimation and Improvement of Radiation Pressure Model for Ikaros
摘要:Expand
An orbit determination of HAYABUSA at Earth swing-by
“HAYABUSA” is a spacecraft to explore the asteroid named “ITOKAWA”. The spacecraft was launched on 9 May,2003 from Uchinoura Space Center by using M-V booster. This spacecraft performed earthExpand
Orbit Determination of Mars Explorer NOZOMI for All the Mission Period
Japanese first Mars explorer NOZOMI, which was launched in July 1998, suffered several problems during the operation period of more than five years. It reached near Mars at the end of 2003, but itExpand
Analysis of orbit determination for MUSES-C
Initial Phase AOCS Operation of Infrared Astronomy Satellite “ AKARI ”
Reported in this paper is the initial phase operation of the attitude and orbit control system (AOCS) of Japanese satellite “AKARI”. AKARI is the first Japanese satellite dedicated to the infraredExpand
A Study on Acceleration Estimation for Solar Sail Ikaros
Abstract Solar sail is expected to be one of the effective propulsion systems for future deep space satellites. JAXA/JSPEC has an experiment plan of solar sail mission “Ikaros”. In this experimentalExpand