Presentation 1996/6/28
Critical Technology of MOON Soft-Landing
Hiroshi Aoki, Shin-ichi Ishikawa, Eijiro Namura, Kouji Yamanaka,
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Abstract(in Japanese) (See Japanese page)
Abstract(in English) NASDA cooperate with ISAS (Institute of Space & Astronautical Science) to plan the MOON orbital observation and landing experiment in early 2000s. Experimental lander is separated from the MOON orbiter, then descends to MOON surface and lands softly, avoiding obstacles on surface. Critical technology of this mission is below, "Direct detection of own relative location, velocity and attitude to MOON surface, then Autonomous and Real-time Control of all parameters in the limitation at target altitude (on MOON surface)". In this paper, Critical Landing Technology is discussed.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) MOON Landing Experiment / Soft-landing / Landing sensor / Throttling Engine
Paper # SANE96-24
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Conference Information
Committee SANE
Conference Date 1996/6/28(1days)
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Paper Information
Registration To Space, Aeronautical and Navigational Electronics (SANE)
Language JPN
Title (in Japanese) (See Japanese page)
Sub Title (in Japanese) (See Japanese page)
Title (in English) Critical Technology of MOON Soft-Landing
Sub Title (in English)
Keyword(1) MOON Landing Experiment
Keyword(2) Soft-landing
Keyword(3) Landing sensor
Keyword(4) Throttling Engine
1st Author's Name Hiroshi Aoki
1st Author's Affiliation National Space Development Agency of Japan (NASDA)()
2nd Author's Name Shin-ichi Ishikawa
2nd Author's Affiliation National Space Development Agency of Japan (NASDA)
3rd Author's Name Eijiro Namura
3rd Author's Affiliation National Space Development Agency of Japan (NASDA)
4th Author's Name Kouji Yamanaka
4th Author's Affiliation National Space Development Agency of Japan (NASDA)
Date 1996/6/28
Paper # SANE96-24
Volume (vol) vol.96
Number (no) 142
Page pp.pp.-
#Pages 8
Date of Issue