Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets
Abstract The precise orbit of the Hayabusa2 spacecraft with respect to asteroid Ryugu is dynamically determined using the data sets collected by the spacecraft’s onboard laser altimeter (LIght Detection And Ranging, LIDAR) and automated image tracking (AIT). The LIDAR range data and the AIT angular...
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Language: | English |
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SpringerOpen
2020-06-01
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Series: | Earth, Planets and Space |
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Online Access: | http://link.springer.com/article/10.1186/s40623-020-01213-2 |
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record_format |
Article |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Keiko Yamamoto Toshimichi Otsubo Koji Matsumoto Hirotomo Noda Noriyuki Namiki Hiroshi Takeuchi Hitoshi Ikeda Makoto Yoshikawa Yukio Yamamoto Hiroki Senshu Takahide Mizuno Naru Hirata Ryuhei Yamada Yoshiaki Ishihara Hiroshi Araki Shinsuke Abe Fumi Yoshida Arika Higuchi Sho Sasaki Shoko Oshigami Seiitsu Tsuruta Kazuyoshi Asari Makoto Shizugami Naoko Ogawa Go Ono Yuya Mimasu Kent Yoshikawa Tadateru Takahashi Yuto Takei Atsushi Fujii Tomohiro Yamaguchi Shota Kikuchi Sei-ichiro Watanabe Satoshi Tanaka Fuyuto Terui Satoru Nakazawa Takanao Saiki Yuichi Tsuda |
spellingShingle |
Keiko Yamamoto Toshimichi Otsubo Koji Matsumoto Hirotomo Noda Noriyuki Namiki Hiroshi Takeuchi Hitoshi Ikeda Makoto Yoshikawa Yukio Yamamoto Hiroki Senshu Takahide Mizuno Naru Hirata Ryuhei Yamada Yoshiaki Ishihara Hiroshi Araki Shinsuke Abe Fumi Yoshida Arika Higuchi Sho Sasaki Shoko Oshigami Seiitsu Tsuruta Kazuyoshi Asari Makoto Shizugami Naoko Ogawa Go Ono Yuya Mimasu Kent Yoshikawa Tadateru Takahashi Yuto Takei Atsushi Fujii Tomohiro Yamaguchi Shota Kikuchi Sei-ichiro Watanabe Satoshi Tanaka Fuyuto Terui Satoru Nakazawa Takanao Saiki Yuichi Tsuda Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets Earth, Planets and Space Hayabusa2 Precise orbit determination LIDAR range data ONC image tracking data GM of Ryugu Solar radiation pressure |
author_facet |
Keiko Yamamoto Toshimichi Otsubo Koji Matsumoto Hirotomo Noda Noriyuki Namiki Hiroshi Takeuchi Hitoshi Ikeda Makoto Yoshikawa Yukio Yamamoto Hiroki Senshu Takahide Mizuno Naru Hirata Ryuhei Yamada Yoshiaki Ishihara Hiroshi Araki Shinsuke Abe Fumi Yoshida Arika Higuchi Sho Sasaki Shoko Oshigami Seiitsu Tsuruta Kazuyoshi Asari Makoto Shizugami Naoko Ogawa Go Ono Yuya Mimasu Kent Yoshikawa Tadateru Takahashi Yuto Takei Atsushi Fujii Tomohiro Yamaguchi Shota Kikuchi Sei-ichiro Watanabe Satoshi Tanaka Fuyuto Terui Satoru Nakazawa Takanao Saiki Yuichi Tsuda |
author_sort |
Keiko Yamamoto |
title |
Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets |
title_short |
Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets |
title_full |
Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets |
title_fullStr |
Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets |
title_full_unstemmed |
Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data sets |
title_sort |
dynamic precise orbit determination of hayabusa2 using laser altimeter (lidar) and image tracking data sets |
publisher |
SpringerOpen |
series |
Earth, Planets and Space |
issn |
1880-5981 |
publishDate |
2020-06-01 |
description |
Abstract The precise orbit of the Hayabusa2 spacecraft with respect to asteroid Ryugu is dynamically determined using the data sets collected by the spacecraft’s onboard laser altimeter (LIght Detection And Ranging, LIDAR) and automated image tracking (AIT). The LIDAR range data and the AIT angular data play complementary roles because LIDAR is sensitive to the line-of-sight direction from Hayabusa2 to Ryugu, while the AIT is sensitive to the directions perpendicular to it. Using LIDAR and AIT, all six components of the initial state vector can be derived stably, which is difficult to achieve using only LIDAR or AIT. The coefficient of solar radiation pressure (SRP) of the Hayabusa2 spacecraft and standard gravitational parameter (GM) of Ryugu can also be estimated in the orbit determination process, by combining multiple orbit arcs at various altitudes. In the process of orbit determination, the Ryugu-fixed coordinate of the center of the LIDAR spot is determined by fitting the range data geometrically to the topography of Ryugu using the Markov Chain Monte Carlo method. Such an approach is effective for realizing the rapid convergence of the solution. The root mean squares of the residuals of the observed minus computed values of the range and brightness-centroid direction of the image are 1.36 m and 0.0270°, respectively. The estimated values of the GM of Ryugu and a correction factor to our initial SRP model are 29.8 ± 0.3 m3/s2 and 1.13 ± 0.16, respectively. |
topic |
Hayabusa2 Precise orbit determination LIDAR range data ONC image tracking data GM of Ryugu Solar radiation pressure |
url |
http://link.springer.com/article/10.1186/s40623-020-01213-2 |
work_keys_str_mv |
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doaj-7af4297eaefe4586843e53dfd00e66362020-11-25T02:27:00ZengSpringerOpenEarth, Planets and Space1880-59812020-06-0172111710.1186/s40623-020-01213-2Dynamic precise orbit determination of Hayabusa2 using laser altimeter (LIDAR) and image tracking data setsKeiko Yamamoto0Toshimichi Otsubo1Koji Matsumoto2Hirotomo Noda3Noriyuki Namiki4Hiroshi Takeuchi5Hitoshi Ikeda6Makoto Yoshikawa7Yukio Yamamoto8Hiroki Senshu9Takahide Mizuno10Naru Hirata11Ryuhei Yamada12Yoshiaki Ishihara13Hiroshi Araki14Shinsuke Abe15Fumi Yoshida16Arika Higuchi17Sho Sasaki18Shoko Oshigami19Seiitsu Tsuruta20Kazuyoshi Asari21Makoto Shizugami22Naoko Ogawa23Go Ono24Yuya Mimasu25Kent Yoshikawa26Tadateru Takahashi27Yuto Takei28Atsushi Fujii29Tomohiro Yamaguchi30Shota Kikuchi31Sei-ichiro Watanabe32Satoshi Tanaka33Fuyuto Terui34Satoru Nakazawa35Takanao Saiki36Yuichi Tsuda37National Astronomical Observatory of JapanHitotsubashi UniversityNational Astronomical Observatory of JapanNational Astronomical Observatory of JapanNational Astronomical Observatory of JapanThe Graduate University for Advanced Studies, SOKENDAIResearch and Development Directorate, JAXA, Japan Aerospace Exploration AgencyThe Graduate University for Advanced Studies, SOKENDAIThe Graduate University for Advanced Studies, SOKENDAIPlanetary Exploration Research Center, Chiba Institute of TechnologyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyThe University of AizuThe University of AizuNational Institute for Environmental StudiesNational Astronomical Observatory of JapanNihon UniversityPlanetary Exploration Research Center, Chiba Institute of TechnologyNational Astronomical Observatory of JapanOsaka UniversityInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyNational Astronomical Observatory of JapanNational Astronomical Observatory of JapanNational Astronomical Observatory of JapanInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyResearch and Development Directorate, JAXA, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyNEC CorporationInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyThe Graduate University for Advanced Studies, SOKENDAIInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyInstitute of Space and Astronautical Science, Japan Aerospace Exploration AgencyThe Graduate University for Advanced Studies, SOKENDAIAbstract The precise orbit of the Hayabusa2 spacecraft with respect to asteroid Ryugu is dynamically determined using the data sets collected by the spacecraft’s onboard laser altimeter (LIght Detection And Ranging, LIDAR) and automated image tracking (AIT). The LIDAR range data and the AIT angular data play complementary roles because LIDAR is sensitive to the line-of-sight direction from Hayabusa2 to Ryugu, while the AIT is sensitive to the directions perpendicular to it. Using LIDAR and AIT, all six components of the initial state vector can be derived stably, which is difficult to achieve using only LIDAR or AIT. The coefficient of solar radiation pressure (SRP) of the Hayabusa2 spacecraft and standard gravitational parameter (GM) of Ryugu can also be estimated in the orbit determination process, by combining multiple orbit arcs at various altitudes. In the process of orbit determination, the Ryugu-fixed coordinate of the center of the LIDAR spot is determined by fitting the range data geometrically to the topography of Ryugu using the Markov Chain Monte Carlo method. Such an approach is effective for realizing the rapid convergence of the solution. The root mean squares of the residuals of the observed minus computed values of the range and brightness-centroid direction of the image are 1.36 m and 0.0270°, respectively. The estimated values of the GM of Ryugu and a correction factor to our initial SRP model are 29.8 ± 0.3 m3/s2 and 1.13 ± 0.16, respectively.http://link.springer.com/article/10.1186/s40623-020-01213-2Hayabusa2Precise orbit determinationLIDAR range dataONC image tracking dataGM of RyuguSolar radiation pressure |