Detection of mass, shape and surface roughness of target asteroid of MUSES-C by LIDAR

被引:14
|
作者
Mukai, T [1 ]
Araki, H
Mizuno, T
Hatanaka, N
Nakamura, AM
Kamei, A
Nakayama, H
Cheng, A
机构
[1] Kobe Univ, Grad Sch Sci & Technol, Kobe, Hyogo 6578501, Japan
[2] Natl Astron Observ, Mizusawa, Japan
[3] Inst Space & Astronaut Sci, Kanagawa 2298510, Japan
[4] Johns Hopkins Univ, Appl Phys Lab, Baltimore, MD 20723 USA
关键词
Gravitational fields;
D O I
10.1016/S0273-1177(02)00141-2
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The LIght Detection And Ranging instrument (LIDAR) is a laser altimeter to be launched with the MUSES-C spacecraft. This ranging function of LIDAR will be applied also to measure the gravitational field around the target asteroid, as well as its shape and surface roughness. Theoretical simulations for the free fall trajectories of the spacecraft suggest that we can estimate the mass of the asteroid with the error of about 5similar to7% by LIDAR. Loboratory measurements of laser backscattering by regolith analogue material showed that the reflected intensity decreased with increasing incident angle relative to normal intensity. The variation becomes weak when the target is covered with regolith compared to the reflected intensity from bedrock. (C) 2002 COSPAR. Published by Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:1231 / 1235
页数:5
相关论文
共 48 条
  • [1] The MUSES-C asteroid sample return mission.
    Zolensky, ME
    METEORITICS & PLANETARY SCIENCE, 2000, 35 : A178 - A178
  • [2] Pole orientation and triaxial ellipsoid shape of (25143) 1998 SF36, a target asteroid of the MUSES-C* mission
    Youhei Ohba
    Masanao Abe
    Sunao Hasegawa
    Masateru Ishiguro
    Tomasz Kwiatkowski
    Francois Colas
    Budi Dermawan
    Akira Fujiwara
    Earth, Planets and Space, 2003, 55 : 341 - 347
  • [3] Image processing for asteroid exploration mission MUSES-C
    Kubota, T
    Hashimoto, T
    Kawaguchi, J
    PROCEEDINGS OF THE 11TH INTERNATIONAL CONFERENCE ON ADVANCED ROBOTICS 2003, VOL 1-3, 2003, : 1221 - 1226
  • [4] Pole orientation and triaxial ellipsoid shape of (25143) 1998 SF36, a target asteroid of the MUSES-C* mission
    Ohba, Y
    Abe, M
    Hasegawa, S
    Ishiguro, M
    Kwiatkowski, T
    Colas, F
    Dermawan, B
    Fujiwara, A
    EARTH PLANETS AND SPACE, 2003, 55 (06): : 341 - 347
  • [5] MUSES-C target asteroid (25143) 1998 SF36: A reddened ordinary chondrite
    Binzel, RP
    Rivkin, AS
    Bus, SJ
    Sunshine, JM
    Burbine, TH
    METEORITICS & PLANETARY SCIENCE, 2001, 36 (08) : 1167 - 1172
  • [6] An autonomous navigation and guidance system for MUSES-C asteroid landing
    Kubota, T
    Hashimoto, T
    Sawai, S
    Kawaguchi, J
    Ninomiya, K
    Uo, M
    Baba, K
    ACTA ASTRONAUTICA, 2003, 52 (2-6) : 125 - 131
  • [7] Role of sample return mission MUSES-C in asteroid study
    Fujiwara, A
    Kawaguchi, J
    Uesugi, KT
    SCIENTIFIC EXPLORATION, PLANETARY PROTECTION, ACTIVE EXPERIMENTS AND DUSTY PLASMAS, 2004, 34 (11): : 2267 - 2269
  • [8] CCD photometry of the MUSES-C mission target: Asteroid (25143) 1998 SF36
    Dermawan, B
    Nakamura, T
    Fukushima, H
    Sato, H
    Yoshida, F
    Sato, Y
    PUBLICATIONS OF THE ASTRONOMICAL SOCIETY OF JAPAN, 2002, 54 (04) : 635 - 640
  • [9] Development of an ion engine system for MUSES-C asteroid exploration mission
    Toki, Kyoichiro
    Kuninaka, Hitoshi
    Funaki, Ikkho
    Shimizu, Yukio
    Nishiyama, Kazutaka
    Shinku/Journal of the Vacuum Society of Japan, 2002, 45 (04) : 336 - 341
  • [10] Navigation, guidance and control of asteroid sample return spacecraft: MUSES-C
    Uo, M
    Baba, K
    Kubota, T
    Hashimoto, T
    Kawaguchi, J
    Sawai, S
    NEC RESEARCH & DEVELOPMENT, 2001, 42 (02): : 188 - 192