Presentation 2007-12-21
Study on Terrain Dependence of a C-Band Pulse Doppler Radar for Lunar Landars
Teppei SATO, Kenji KISHIMOTO, Tomohiko SAKAI, Seisuke FUKUDA, Takahide MIZUNO,
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Abstract(in Japanese) (See Japanese page)
Abstract(in English) An accurate measurement of velocity is necessary for scientific observation using a lunar and a planetary lander that landing ambiguity is less than 100m. A landing radar is a sensor which measure an altitude and velocity of a space craft with C-band microwave pulse. This report describes that the dependance of terrain for velocity measurement and the result of field experiment using a helicopter.
Keyword(in Japanese) (See Japanese page)
Keyword(in English) landing radar / doppler / pulse radar / lunur exploration / lunar mission
Paper # SANE2007-98
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Conference Information
Committee SANE
Conference Date 2007/12/14(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) Study on Terrain Dependence of a C-Band Pulse Doppler Radar for Lunar Landars
Sub Title (in English)
Keyword(1) landing radar
Keyword(2) doppler
Keyword(3) pulse radar
Keyword(4) lunur exploration
Keyword(5) lunar mission
1st Author's Name Teppei SATO
1st Author's Affiliation Tokyo University of Science:Meiji Univ.()
2nd Author's Name Kenji KISHIMOTO
2nd Author's Affiliation / Institute of Space and Astronautical Science
3rd Author's Name Tomohiko SAKAI
3rd Author's Affiliation Institute of Space and Astronautical Science
4th Author's Name Seisuke FUKUDA
4th Author's Affiliation Institute of Space and Astronautical Science
5th Author's Name Takahide MIZUNO
5th Author's Affiliation
Date 2007-12-21
Paper # SANE2007-98
Volume (vol) vol.107
Number (no) 407
Page pp.pp.-
#Pages 6
Date of Issue