Trajectory Analysis of the Hayabusa2 Capsule from a Single Airborne Observation
The reentry trajectory of the Hayabusa2 capsule has been measured using a single video stream captured during the Australian Airborne Observation of the Hayabusa2 capsule. A new analysis methodology was required, and developed, to enable the trajectory to be determined from a single viewpoint. The m...
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Veröffentlicht in: | Journal of spacecraft and rockets 2024-01, Vol.61 (1), p.173-180 |
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description | The reentry trajectory of the Hayabusa2 capsule has been measured using a single video stream captured during the Australian Airborne Observation of the Hayabusa2 capsule. A new analysis methodology was required, and developed, to enable the trajectory to be determined from a single viewpoint. The method developed used the star-field background visible in the video stream, combined with the aircraft Global Positioning System data, to establish lines of sight along which the capsule was measured in time. A set of common sense criteria including altitude and velocity limits were then used to exclude impossible trajectories. The remaining trajectories were then examined and evaluated using a least-squares fitting routine to analyze candidate ballistic trajectories. The trajectories were ranked based on the fit parameter, enabling the determination of the single most likely trajectory and a family of most probable trajectories. The most probable Hayabusa2 capsule trajectory inferred from the measurements passed 10 km west of Coober Pedy and traveled at a heading of 150 deg. Evaluation of other highly probable trajectories showed they all passed Coober Pedy at a similar distance; however, they tended toward a slightly higher heading, approaching 155 deg. The distance between the measurement aircraft and the capsule remained relatively constant at approximately 180 km throughout the measurement period. This work demonstrates a new method for determining the trajectory of an object measured with a star-field background. Importantly, we have used this to establish the Hayabusa2 reentry capsule trajectory, and hence the distance from our aircraft, which will allow the detailed analysis of our spectral data. |
doi_str_mv | 10.2514/1.A35719 |
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A new analysis methodology was required, and developed, to enable the trajectory to be determined from a single viewpoint. The method developed used the star-field background visible in the video stream, combined with the aircraft Global Positioning System data, to establish lines of sight along which the capsule was measured in time. A set of common sense criteria including altitude and velocity limits were then used to exclude impossible trajectories. The remaining trajectories were then examined and evaluated using a least-squares fitting routine to analyze candidate ballistic trajectories. The trajectories were ranked based on the fit parameter, enabling the determination of the single most likely trajectory and a family of most probable trajectories. The most probable Hayabusa2 capsule trajectory inferred from the measurements passed 10 km west of Coober Pedy and traveled at a heading of 150 deg. Evaluation of other highly probable trajectories showed they all passed Coober Pedy at a similar distance; however, they tended toward a slightly higher heading, approaching 155 deg. The distance between the measurement aircraft and the capsule remained relatively constant at approximately 180 km throughout the measurement period. This work demonstrates a new method for determining the trajectory of an object measured with a star-field background. Importantly, we have used this to establish the Hayabusa2 reentry capsule trajectory, and hence the distance from our aircraft, which will allow the detailed analysis of our spectral data.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/1.A35719</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Airborne observation ; Aircraft ; Ballistic trajectories ; Evaluation ; Japanese spacecraft ; Reentry trajectories ; Reentry vehicles ; Space capsules ; Trajectory analysis ; Trajectory measurement ; Video data</subject><ispartof>Journal of spacecraft and rockets, 2024-01, Vol.61 (1), p.173-180</ispartof><rights>Copyright © 2023 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at ; employ the eISSN to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2023 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-6794 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-a246t-ed4da8e470de2020cdc0bf41756f24ad86df5420146acb1374f171a3dcc7922a3</cites><orcidid>0000-0003-0625-2455</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27901,27902</link.rule.ids></links><search><creatorcontrib>Zander, Fabian</creatorcontrib><creatorcontrib>Buttsworth, David R.</creatorcontrib><creatorcontrib>Birch, Byrenn</creatorcontrib><creatorcontrib>Payne, Allan</creatorcontrib><title>Trajectory Analysis of the Hayabusa2 Capsule from a Single Airborne Observation</title><title>Journal of spacecraft and rockets</title><description>The reentry trajectory of the Hayabusa2 capsule has been measured using a single video stream captured during the Australian Airborne Observation of the Hayabusa2 capsule. A new analysis methodology was required, and developed, to enable the trajectory to be determined from a single viewpoint. The method developed used the star-field background visible in the video stream, combined with the aircraft Global Positioning System data, to establish lines of sight along which the capsule was measured in time. A set of common sense criteria including altitude and velocity limits were then used to exclude impossible trajectories. The remaining trajectories were then examined and evaluated using a least-squares fitting routine to analyze candidate ballistic trajectories. The trajectories were ranked based on the fit parameter, enabling the determination of the single most likely trajectory and a family of most probable trajectories. The most probable Hayabusa2 capsule trajectory inferred from the measurements passed 10 km west of Coober Pedy and traveled at a heading of 150 deg. Evaluation of other highly probable trajectories showed they all passed Coober Pedy at a similar distance; however, they tended toward a slightly higher heading, approaching 155 deg. The distance between the measurement aircraft and the capsule remained relatively constant at approximately 180 km throughout the measurement period. This work demonstrates a new method for determining the trajectory of an object measured with a star-field background. Importantly, we have used this to establish the Hayabusa2 reentry capsule trajectory, and hence the distance from our aircraft, which will allow the detailed analysis of our spectral data.</description><subject>Airborne observation</subject><subject>Aircraft</subject><subject>Ballistic trajectories</subject><subject>Evaluation</subject><subject>Japanese spacecraft</subject><subject>Reentry trajectories</subject><subject>Reentry vehicles</subject><subject>Space capsules</subject><subject>Trajectory analysis</subject><subject>Trajectory measurement</subject><subject>Video data</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><recordid>eNplkEtLw0AYRQdRsFbBnzAggpvovKdZhqJWKHRhXQ9f5qEpbabOJEL-vZEILlxdLhwO3IvQNSX3TFLxQO8rLjUtT9CMSs4LpUtximaEMFYIJck5ush5RwhVC1XO0GabYOdtF9OAqxb2Q24yjgF3Hx6vYIC6z8DwEo6533scUjxgwK9N-z62qkl1TK3Hmzr79AVdE9tLdBZgn_3Vb87R29Pjdrkq1pvnl2W1LoAJ1RXeCQcLLzRxnhFGrLOkDoJqqQIT4BbKBSkYoUKBrSnXIlBNgTtrdckY8Dm6mbzHFD97nzuzi30aB2TDytGouCR8pO4myqaYc_LBHFNzgDQYSszPXYaa6a4RvZ1QaAD-ZP-4b-A3ZzI</recordid><startdate>202401</startdate><enddate>202401</enddate><creator>Zander, Fabian</creator><creator>Buttsworth, David R.</creator><creator>Birch, Byrenn</creator><creator>Payne, Allan</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope><orcidid>https://orcid.org/0000-0003-0625-2455</orcidid></search><sort><creationdate>202401</creationdate><title>Trajectory Analysis of the Hayabusa2 Capsule from a Single Airborne Observation</title><author>Zander, Fabian ; Buttsworth, David R. ; Birch, Byrenn ; Payne, Allan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a246t-ed4da8e470de2020cdc0bf41756f24ad86df5420146acb1374f171a3dcc7922a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Airborne observation</topic><topic>Aircraft</topic><topic>Ballistic trajectories</topic><topic>Evaluation</topic><topic>Japanese spacecraft</topic><topic>Reentry trajectories</topic><topic>Reentry vehicles</topic><topic>Space capsules</topic><topic>Trajectory analysis</topic><topic>Trajectory measurement</topic><topic>Video data</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zander, Fabian</creatorcontrib><creatorcontrib>Buttsworth, David R.</creatorcontrib><creatorcontrib>Birch, Byrenn</creatorcontrib><creatorcontrib>Payne, Allan</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of spacecraft and rockets</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zander, Fabian</au><au>Buttsworth, David R.</au><au>Birch, Byrenn</au><au>Payne, Allan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Trajectory Analysis of the Hayabusa2 Capsule from a Single Airborne Observation</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>2024-01</date><risdate>2024</risdate><volume>61</volume><issue>1</issue><spage>173</spage><epage>180</epage><pages>173-180</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>The reentry trajectory of the Hayabusa2 capsule has been measured using a single video stream captured during the Australian Airborne Observation of the Hayabusa2 capsule. A new analysis methodology was required, and developed, to enable the trajectory to be determined from a single viewpoint. The method developed used the star-field background visible in the video stream, combined with the aircraft Global Positioning System data, to establish lines of sight along which the capsule was measured in time. A set of common sense criteria including altitude and velocity limits were then used to exclude impossible trajectories. The remaining trajectories were then examined and evaluated using a least-squares fitting routine to analyze candidate ballistic trajectories. The trajectories were ranked based on the fit parameter, enabling the determination of the single most likely trajectory and a family of most probable trajectories. The most probable Hayabusa2 capsule trajectory inferred from the measurements passed 10 km west of Coober Pedy and traveled at a heading of 150 deg. Evaluation of other highly probable trajectories showed they all passed Coober Pedy at a similar distance; however, they tended toward a slightly higher heading, approaching 155 deg. The distance between the measurement aircraft and the capsule remained relatively constant at approximately 180 km throughout the measurement period. This work demonstrates a new method for determining the trajectory of an object measured with a star-field background. Importantly, we have used this to establish the Hayabusa2 reentry capsule trajectory, and hence the distance from our aircraft, which will allow the detailed analysis of our spectral data.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.A35719</doi><tpages>8</tpages><orcidid>https://orcid.org/0000-0003-0625-2455</orcidid></addata></record> |
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source | Alma/SFX Local Collection |
subjects | Airborne observation Aircraft Ballistic trajectories Evaluation Japanese spacecraft Reentry trajectories Reentry vehicles Space capsules Trajectory analysis Trajectory measurement Video data |
title | Trajectory Analysis of the Hayabusa2 Capsule from a Single Airborne Observation |
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