Flight result of SDS-1 and development of SDS-4 in JAXA(Technical Session,ICSANE 2011(International Conference on Space, Aeronautical and Navigational Electronics 2011))
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概要
- 論文の詳細を見る
Small Demonstration Satellite (SDS) program provides useful standard small satellite platforms to demonstrate advanced space technology with timely launch opportunity. SDS-1 is the first satellite in this program. It has three main mission components: 1.Multi-mode Integrated Transponder, 2.Space-wire demonstration Module and super high sensitivity accelerometer for future gravitational wave observation, and 3.Advanced Micro processing In-orbit experiment equipment. The satellite was launched successfully by H-IIA launch vehicle in January 2009. Now all missions are successful and excellent results are obtained including world's first achievement. SDS-4 project was initiated in 2009 and planned to be launched in 2012. The main missions of the SDS-4 are the demonstration of Space-based Automatic Identification System Experiment, Quartz Crystal Microbalance for monitoring contamination environment around the spacecraft, Flat-plate Heat Pipe Experiment, and In-flight experiment of Space materials using THERME which is developed by the JAXA-CNES joint research program.
- 2011-10-10
著者
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Ohtani Takashi
Japan Aerospace Exploration Agency (jaxa)
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Nakamura Yosuke
Japan Aerospace Exploration Agency
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NISHIJO Kunitoshi
Japan Aerospace Exploration Agency
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TAKAHASHI Yasuyuki
Japan Aerospace Exploration Agency
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INOUE Koichi
Japan Aerospace Exploration Agency
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HIRAKO Keiishi
Japan Aerospace Exploration Agency
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Ohtani Takashi
Japan Aerospace Exploration Agency
関連論文
- System Identification Using Impulse Response Including Initial States
- ROBUST ATTITUDE CONTROL USING MU-SYNTHESIS FOR THE LARGE FLEXIBLE SATELLITE ETS-VIII
- Flight result of SDS-1 and development of SDS-4 in JAXA(Technical Session,ICSANE 2011(International Conference on Space, Aeronautical and Navigational Electronics 2011))
- In-orbit Control Experiment on ETS-VIII Spacecraft
- Robust Attitude Control Using Mu-Synthesis for the Large Flexible Satellite ETS-VIII