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Correction to: Orbit insertion strategy of Hayabusa2’s rover with large release uncertainty around the asteroid Ryugu

Show Author's information Yusuke Oki1( )Kent Yoshikawa2Hiroshi Takeuchi2Shota Kikuchi2Hitosi Ikeda2Daniel J. Scheeres3Jay W. McMahon3Junichiro Kawaguchi2Yuto Takei2Yuya Mimasu2Naoko Ogawa2Go Ono2Fuyuto Terui2Manabu Yamada4Toru Kouyama5Shingo Kameda6Kazuya Yoshida7Kenji Nagaoka8Tetsuo Yoshimitsu2Takanao Saiki2Yuichi Tsuda2
Japan Aerospace Exploration Agency, Tsukuba 305-8505, Japan
Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
University of Colorado, Boulder, CO 80309, USA
Planetary Exploration Research Center, Chiba Institute of Technology, Narashino 275-0016, Japan
National Institute of Advanced Industrial Science and Technology, Koto-ku 135-0064, Japan
Rikkyo University, Toshima-ku 171-8501, Japan
Department of Aerospace Engineering, Tohoku University, Sendai 980-8579, Japan
Kyushu Institute of Technology, Kitakyusyu 804-8550, Japan
Keywords: solar radiation pressure, augmented elliptic Hill three-body problem, gravitational irregularity
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Published: 10 February 2021
Issue date: June 2021

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