LIDAR for Asteroid Explore Hayabusa: Development and on Board Evaluation
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- Mizuno Takahide
- 宇宙航空研究開発機構宇宙科学研究本部
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- Tsuno Katsuhiko
- NEC東芝スペースシステム(株)
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- Okumura Eisuke
- NEC東芝スペースシステム(株)
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- Nakayama Michio
- (株)東芝
Bibliographic Information
- Other Title
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- 小惑星探査機はやぶさ搭載用レーザ高度計:機器開発とその実運用結果報告
- ショウワクセイ タンサキ ハヤブサ トウサイヨウ レーザ コウドケイ キキ カイハツ ト ソノ ジツ ウンヨウ ケッカ ホウコク
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Abstract
Hayabusa, launched May 2003, is the first Japanese spacecraft to explore the small asteroid Itokawa (1998SF36) and touched down on Itokawa twice to sample of the surface material. LIDAR (LIght Detection And Ranging) is an important navigation sensor for the asteroid explorer to measure distance between the spacecraft and the asteroid. Since it is carried in a planetary exploration spacecraft, the weight of LIDAR is very lightweight of 3.7kg. In the rendezvous and touchdown operation, LIDAR supplied the ranging data to the spacecraft navigation system to approach Itokawa down to 50m and its total shots number of laser pulse was more than 4 million. The composition and basic performance of LIDAR are explained and this paper also reports the ranging data at the time of landing to asteroid Itokawa of the autumn of 2005.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 54 (634), 514-521, 2006
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679446963840
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- NII Article ID
- 10018429152
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 8580061
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed