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Volume 5
,
Issue 2
Astrodynamics
2021, 5
(
2
): 183
https://doi.org/10.1007/s42064-021-0100-6
Erratum
|
Issue
|
Published:
10 February 2021
Correction to: Orbit insertion strategy of Hayabusa2’s rover with large release uncertainty around the asteroid Ryugu
Show Author's Information
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Yusuke Oki
1
(
)
,
Kent Yoshikawa
2
,
Hiroshi Takeuchi
2
,
Shota Kikuchi
2
,
Hitosi Ikeda
2
,
Daniel J. Scheeres
3
,
Jay W. McMahon
3
,
Junichiro Kawaguchi
2
,
Yuto Takei
2
,
Yuya Mimasu
2
,
Naoko Ogawa
2
,
Go Ono
2
,
Fuyuto Terui
2
,
Manabu Yamada
4
,
Toru Kouyama
5
,
Shingo Kameda
6
,
Kazuya Yoshida
7
,
Kenji Nagaoka
8
,
Tetsuo Yoshimitsu
2
,
Takanao Saiki
2
,
Yuichi Tsuda
2
1
Japan Aerospace Exploration Agency
,
Tsukuba
305-8505
,
Japan
2
Japan Aerospace Exploration Agency
,
Sagamihara
252-5210
,
Japan
3
University of Colorado
,
Boulder
,
CO
80309
,
USA
4
Planetary Exploration Research Center, Chiba Institute of Technology
,
Narashino
275-0016
,
Japan
5
National Institute of Advanced Industrial Science and Technology
,
Koto-ku
135-0064
,
Japan
6
Rikkyo University
,
Toshima-ku
171-8501
,
Japan
7
Department of Aerospace Engineering
,
Tohoku University
,
Sendai
980-8579
,
Japan
8
Kyushu Institute of Technology
,
Kitakyusyu
804-8550
,
Japan
Keywords:
solar radiation pressure,
augmented elliptic Hill three-body problem,
gravitational irregularity
The online version of the original article can be found at
https://doi.org/10.1007/s42064-020-0080-y
Cite this article:
Oki Y, Yoshikawa K, Takeuchi H, et al.
Correction to: Orbit insertion strategy of Hayabusa2’s rover with large release uncertainty around the asteroid Ryugu.
Astrodynamics
,
2021, 5(2): 183.
https://doi.org/10.1007/s42064-021-0100-6
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About this article
Correction to: Orbit insertion strategy of Hayabusa2’s rover with large release uncertainty around the asteroid Ryugu
Show Author's information
Hide Author's Information
Yusuke Oki
1
(
)
,
Kent Yoshikawa
2
,
Hiroshi Takeuchi
2
,
Shota Kikuchi
2
,
Hitosi Ikeda
2
,
Daniel J. Scheeres
3
,
Jay W. McMahon
3
,
Junichiro Kawaguchi
2
,
Yuto Takei
2
,
Yuya Mimasu
2
,
Naoko Ogawa
2
,
Go Ono
2
,
Fuyuto Terui
2
,
Manabu Yamada
4
,
Toru Kouyama
5
,
Shingo Kameda
6
,
Kazuya Yoshida
7
,
Kenji Nagaoka
8
,
Tetsuo Yoshimitsu
2
,
Takanao Saiki
2
,
Yuichi Tsuda
2
1
Japan Aerospace Exploration Agency
,
Tsukuba
305-8505
,
Japan
2
Japan Aerospace Exploration Agency
,
Sagamihara
252-5210
,
Japan
3
University of Colorado
,
Boulder
,
CO
80309
,
USA
4
Planetary Exploration Research Center, Chiba Institute of Technology
,
Narashino
275-0016
,
Japan
5
National Institute of Advanced Industrial Science and Technology
,
Koto-ku
135-0064
,
Japan
6
Rikkyo University
,
Toshima-ku
171-8501
,
Japan
7
Department of Aerospace Engineering
,
Tohoku University
,
Sendai
980-8579
,
Japan
8
Kyushu Institute of Technology
,
Kitakyusyu
804-8550
,
Japan
Keywords:
solar radiation pressure, augmented elliptic Hill three-body problem, gravitational irregularity
About this article
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Published:
10 February 2021
Issue date: June 2021
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© The Author(s) 2021
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