MUSES-C touch-down simulation on the ground

Kazuya Yoshida; Takashi Kubota; Shujiro Sawai; Akira Fujiwara; Masashi Uo

MUSES-C touch-down simulation on the ground

Kazuya Yoshida, Takashi Kubota, Shujiro Sawai, Akira Fujiwara, Masashi Uo

工学研究科・航空宇宙工学専攻

研究成果: Conference article › 査読

14 被引用数 (Scopus)

抄録

The MUSES-C spacecraft, under the development by the Institute of Space and Astronautical Science (ISAS) of Japan for the asteroid sample-return mission, will make dynamic touch-down with the target asteroid when it acquires samples. The touch-down behavior is studied with simulations based on the multi-body dynamics with a friction model. Hardware experiments are carried out to verify the simulation model and evaluate the performance of the contact detector.

本文言語	English
ページ（範囲）	481-490
ページ数	10
ジャーナル	Advances in the Astronautical Sciences
巻	108 I
出版ステータス	Published - 2001 12月 1
イベント	Proceedings of the AAS/AIAA Space Flight Mechanics Meeting - Santa Barbara, CA, United States 継続期間: 2001 2月 11 → 2001 2月 15

ASJC Scopus subject areas

航空宇宙工学
宇宙惑星科学

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引用スタイル

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abstract = "The MUSES-C spacecraft, under the development by the Institute of Space and Astronautical Science (ISAS) of Japan for the asteroid sample-return mission, will make dynamic touch-down with the target asteroid when it acquires samples. The touch-down behavior is studied with simulations based on the multi-body dynamics with a friction model. Hardware experiments are carried out to verify the simulation model and evaluate the performance of the contact detector.",

author = "Kazuya Yoshida and Takashi Kubota and Shujiro Sawai and Akira Fujiwara and Masashi Uo",

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note = "Proceedings of the AAS/AIAA Space Flight Mechanics Meeting ; Conference date: 11-02-2001 Through 15-02-2001",

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AU - Yoshida, Kazuya

AU - Kubota, Takashi

AU - Sawai, Shujiro

AU - Fujiwara, Akira

AU - Uo, Masashi

PY - 2001/12/1

Y1 - 2001/12/1

N2 - The MUSES-C spacecraft, under the development by the Institute of Space and Astronautical Science (ISAS) of Japan for the asteroid sample-return mission, will make dynamic touch-down with the target asteroid when it acquires samples. The touch-down behavior is studied with simulations based on the multi-body dynamics with a friction model. Hardware experiments are carried out to verify the simulation model and evaluate the performance of the contact detector.

AB - The MUSES-C spacecraft, under the development by the Institute of Space and Astronautical Science (ISAS) of Japan for the asteroid sample-return mission, will make dynamic touch-down with the target asteroid when it acquires samples. The touch-down behavior is studied with simulations based on the multi-body dynamics with a friction model. Hardware experiments are carried out to verify the simulation model and evaluate the performance of the contact detector.

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M3 - Conference article

AN - SCOPUS:0035729733

SN - 1081-6003

VL - 108 I

SP - 481

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JO - Advances in the Astronautical Sciences

JF - Advances in the Astronautical Sciences

T2 - Proceedings of the AAS/AIAA Space Flight Mechanics Meeting

Y2 - 11 February 2001 through 15 February 2001

ER -

MUSES-C touch-down simulation on the ground

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