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Astrodynamics

Article Title

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

Authors

Yusuke Oki, Japan Aerospace Exploration Agency, Tsukuba 305-8505, Japan
Kent Yoshikawa, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Hiroshi Takeuchi, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Shota Kikuchi, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Hitosi Ikeda, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Daniel J. Scheeres, University of Colorado, Boulder, CO 80309, USA
Jay W. McMahon, University of Colorado, Boulder, CO 80309, USA
Junichiro Kawaguchi, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Yuto Takei, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Yuya Mimasu, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Naoko Ogawa, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Go Ono, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Fuyuto Terui, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Manabu Yamada, Planetary Exploration Research Center, Chiba Institute of Technology, Narashino 275-0016, Japan
Toru Kouyama, National Institute of Advanced Industrial Science and Technology, Koto-ku 135-0064, Japan
Shingo Kameda, Rikkyo University, Toshima-ku 171-8501, Japan
Kazuya Yoshida, Department of Aerospace Engineering, Tohoku University, Sendai 980-8579, Japan
Kenji Nagaoka, Kyushu Institute of Technology, Kitakyusyu 804-8550, Japan
Tetsuo Yoshimitsu, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan
Takanao Saiki, Japan Aerospace Exploration Agency, Sagamihara 252-5210, Japan

Publisher

Tsinghua University Press

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