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Erratum

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

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
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The online version of the original article can be found at:
https://doi.org/10.1007/s42064-020-0080-y

Keywords

solar radiation pressureaugmented elliptic Hill three-body problemgravitational irregularity

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Astrodynamics
Volume 5 Issue 2,
June 2021
Pages 183-183
DOI: 10.1007/s42064-021-0100-6

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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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Published: 10 February 2021
© The Author(s) 2021