Adaptive Position and Attitude-Tracking Controller for Satellite Proximity Operations Using Dual Quaternions
This paper proposes a nonlinear adaptive position and attitude-tracking controller for satellite proximity operations between a target and a chaser satellite. The controller requires no information about the mass and inertia matrix of the chaser satellite and takes into account the gravitational acc...
Gespeichert in:
| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2015-04, Vol.38 (4), p.566-577 |
|---|---|
| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| container_end_page | 577 |
|---|---|
| container_issue | 4 |
| container_start_page | 566 |
| container_title | Journal of guidance, control, and dynamics |
| container_volume | 38 |
| creator | Filipe, Nuno Tsiotras, Panagiotis |
| description | This paper proposes a nonlinear adaptive position and attitude-tracking controller for satellite proximity operations between a target and a chaser satellite. The controller requires no information about the mass and inertia matrix of the chaser satellite and takes into account the gravitational acceleration, the gravity-gradient torque, the perturbing acceleration due to Earth's oblateness, and constant (but otherwise unknown) disturbance forces and torques. Sufficient conditions to identify the mass and inertia matrix of the chaser satellite are also given. The controller is shown to ensure almost global asymptotical stability of the translational and rotational position and velocity tracking errors. Unit dual quaternions are used to simultaneously represent the absolute and relative attitude and position of the target and chaser satellites. The analogies between quaternions and dual quaternions are explored in the development of the controller. Presented as Paper 2013-5173 at the AIAA Guidance, Navigation, and Control Conference, Boston, MA, 19-22 August 2013 |
| doi_str_mv | 10.2514/1.G000054 |
| format | Article |
| fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_1677914678</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>2494813196</sourcerecordid><originalsourceid>FETCH-LOGICAL-c353t-3ef4c7008b792daa445f412a767e7a9f66b2256faa7e4f27aef962ce9f25e5cb3</originalsourceid><addsrcrecordid>eNp9kU1LAzEYhIMoWKsH_0HAix625jubY6lahUIV2_OS7iaSut2sSVbsv3eX9uTB9zLw8swwMABcYzQhHLN7PJmj_jg7ASPMKc1onrNTMEKS4owjhc7BRYxbhDAVWI5APa10m9y3ga8-uuR8A3VTwWlKLnWVyVZBl5-u-YAz36Tg69oEaH2A7zqZunap9wX_43Yu7eGyNUEPERGu4-B56HQN37oeDc3wvgRnVtfRXB11DNZPj6vZc7ZYzl9m00VWUk5TRo1lpUQo30hFKq0Z45ZhoqWQRmplhdgQwoXVWhpmidTGKkFKoyzhhpcbOga3h9w2-K_OxFTsXCz7vroxvosFFlIqzITMe_TmD7r1XWj6dgVhiuWYYiX-o7AQhAnF8JB1d6DK4GMMxhZtcDsd9gVGxbBOgYvjOvQXp9uB1Q</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>1662469418</pqid></control><display><type>article</type><title>Adaptive Position and Attitude-Tracking Controller for Satellite Proximity Operations Using Dual Quaternions</title><source>Alma/SFX Local Collection</source><creator>Filipe, Nuno ; Tsiotras, Panagiotis</creator><creatorcontrib>Filipe, Nuno ; Tsiotras, Panagiotis</creatorcontrib><description>This paper proposes a nonlinear adaptive position and attitude-tracking controller for satellite proximity operations between a target and a chaser satellite. The controller requires no information about the mass and inertia matrix of the chaser satellite and takes into account the gravitational acceleration, the gravity-gradient torque, the perturbing acceleration due to Earth's oblateness, and constant (but otherwise unknown) disturbance forces and torques. Sufficient conditions to identify the mass and inertia matrix of the chaser satellite are also given. The controller is shown to ensure almost global asymptotical stability of the translational and rotational position and velocity tracking errors. Unit dual quaternions are used to simultaneously represent the absolute and relative attitude and position of the target and chaser satellites. The analogies between quaternions and dual quaternions are explored in the development of the controller. Presented as Paper 2013-5173 at the AIAA Guidance, Navigation, and Control Conference, Boston, MA, 19-22 August 2013</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G000054</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Acceleration ; Adaptive control ; Adaptive control systems ; Aerospace engineering ; Asymptotic properties ; Control stability ; Controllers ; Inertia ; Proximity ; Quaternions ; Satellite attitude control ; Satellite tracking ; Satellites ; Torque ; Tracking control ; Tracking errors ; Velocity</subject><ispartof>Journal of guidance, control, and dynamics, 2015-04, Vol.38 (4), p.566-577</ispartof><rights>Copyright © 2013 by N. Filipe and P. Tsiotras. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code 1533-3884/14 and $10.00 in correspondence with the CCC.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c353t-3ef4c7008b792daa445f412a767e7a9f66b2256faa7e4f27aef962ce9f25e5cb3</citedby><cites>FETCH-LOGICAL-c353t-3ef4c7008b792daa445f412a767e7a9f66b2256faa7e4f27aef962ce9f25e5cb3</cites></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>Filipe, Nuno</creatorcontrib><creatorcontrib>Tsiotras, Panagiotis</creatorcontrib><title>Adaptive Position and Attitude-Tracking Controller for Satellite Proximity Operations Using Dual Quaternions</title><title>Journal of guidance, control, and dynamics</title><description>This paper proposes a nonlinear adaptive position and attitude-tracking controller for satellite proximity operations between a target and a chaser satellite. The controller requires no information about the mass and inertia matrix of the chaser satellite and takes into account the gravitational acceleration, the gravity-gradient torque, the perturbing acceleration due to Earth's oblateness, and constant (but otherwise unknown) disturbance forces and torques. Sufficient conditions to identify the mass and inertia matrix of the chaser satellite are also given. The controller is shown to ensure almost global asymptotical stability of the translational and rotational position and velocity tracking errors. Unit dual quaternions are used to simultaneously represent the absolute and relative attitude and position of the target and chaser satellites. The analogies between quaternions and dual quaternions are explored in the development of the controller. Presented as Paper 2013-5173 at the AIAA Guidance, Navigation, and Control Conference, Boston, MA, 19-22 August 2013</description><subject>Acceleration</subject><subject>Adaptive control</subject><subject>Adaptive control systems</subject><subject>Aerospace engineering</subject><subject>Asymptotic properties</subject><subject>Control stability</subject><subject>Controllers</subject><subject>Inertia</subject><subject>Proximity</subject><subject>Quaternions</subject><subject>Satellite attitude control</subject><subject>Satellite tracking</subject><subject>Satellites</subject><subject>Torque</subject><subject>Tracking control</subject><subject>Tracking errors</subject><subject>Velocity</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><recordid>eNp9kU1LAzEYhIMoWKsH_0HAix625jubY6lahUIV2_OS7iaSut2sSVbsv3eX9uTB9zLw8swwMABcYzQhHLN7PJmj_jg7ASPMKc1onrNTMEKS4owjhc7BRYxbhDAVWI5APa10m9y3ga8-uuR8A3VTwWlKLnWVyVZBl5-u-YAz36Tg69oEaH2A7zqZunap9wX_43Yu7eGyNUEPERGu4-B56HQN37oeDc3wvgRnVtfRXB11DNZPj6vZc7ZYzl9m00VWUk5TRo1lpUQo30hFKq0Z45ZhoqWQRmplhdgQwoXVWhpmidTGKkFKoyzhhpcbOga3h9w2-K_OxFTsXCz7vroxvosFFlIqzITMe_TmD7r1XWj6dgVhiuWYYiX-o7AQhAnF8JB1d6DK4GMMxhZtcDsd9gVGxbBOgYvjOvQXp9uB1Q</recordid><startdate>20150401</startdate><enddate>20150401</enddate><creator>Filipe, Nuno</creator><creator>Tsiotras, Panagiotis</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope></search><sort><creationdate>20150401</creationdate><title>Adaptive Position and Attitude-Tracking Controller for Satellite Proximity Operations Using Dual Quaternions</title><author>Filipe, Nuno ; Tsiotras, Panagiotis</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c353t-3ef4c7008b792daa445f412a767e7a9f66b2256faa7e4f27aef962ce9f25e5cb3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2015</creationdate><topic>Acceleration</topic><topic>Adaptive control</topic><topic>Adaptive control systems</topic><topic>Aerospace engineering</topic><topic>Asymptotic properties</topic><topic>Control stability</topic><topic>Controllers</topic><topic>Inertia</topic><topic>Proximity</topic><topic>Quaternions</topic><topic>Satellite attitude control</topic><topic>Satellite tracking</topic><topic>Satellites</topic><topic>Torque</topic><topic>Tracking control</topic><topic>Tracking errors</topic><topic>Velocity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Filipe, Nuno</creatorcontrib><creatorcontrib>Tsiotras, Panagiotis</creatorcontrib><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>ProQuest Computer Science Collection</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Computer and Information Systems Abstracts Academic</collection><collection>Computer and Information Systems Abstracts Professional</collection><jtitle>Journal of guidance, control, and dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Filipe, Nuno</au><au>Tsiotras, Panagiotis</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Adaptive Position and Attitude-Tracking Controller for Satellite Proximity Operations Using Dual Quaternions</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2015-04-01</date><risdate>2015</risdate><volume>38</volume><issue>4</issue><spage>566</spage><epage>577</epage><pages>566-577</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>This paper proposes a nonlinear adaptive position and attitude-tracking controller for satellite proximity operations between a target and a chaser satellite. The controller requires no information about the mass and inertia matrix of the chaser satellite and takes into account the gravitational acceleration, the gravity-gradient torque, the perturbing acceleration due to Earth's oblateness, and constant (but otherwise unknown) disturbance forces and torques. Sufficient conditions to identify the mass and inertia matrix of the chaser satellite are also given. The controller is shown to ensure almost global asymptotical stability of the translational and rotational position and velocity tracking errors. Unit dual quaternions are used to simultaneously represent the absolute and relative attitude and position of the target and chaser satellites. The analogies between quaternions and dual quaternions are explored in the development of the controller. Presented as Paper 2013-5173 at the AIAA Guidance, Navigation, and Control Conference, Boston, MA, 19-22 August 2013</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.G000054</doi><tpages>12</tpages><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext |
| identifier | ISSN: 0731-5090 |
| ispartof | Journal of guidance, control, and dynamics, 2015-04, Vol.38 (4), p.566-577 |
| issn | 0731-5090 1533-3884 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_1677914678 |
| source | Alma/SFX Local Collection |
| subjects | Acceleration Adaptive control Adaptive control systems Aerospace engineering Asymptotic properties Control stability Controllers Inertia Proximity Quaternions Satellite attitude control Satellite tracking Satellites Torque Tracking control Tracking errors Velocity |
| title | Adaptive Position and Attitude-Tracking Controller for Satellite Proximity Operations Using Dual Quaternions |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-02T14%3A22%3A07IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Adaptive%20Position%20and%20Attitude-Tracking%20Controller%20for%20Satellite%20Proximity%20Operations%20Using%20Dual%20Quaternions&rft.jtitle=Journal%20of%20guidance,%20control,%20and%20dynamics&rft.au=Filipe,%20Nuno&rft.date=2015-04-01&rft.volume=38&rft.issue=4&rft.spage=566&rft.epage=577&rft.pages=566-577&rft.issn=0731-5090&rft.eissn=1533-3884&rft_id=info:doi/10.2514/1.G000054&rft_dat=%3Cproquest_cross%3E2494813196%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=1662469418&rft_id=info:pmid/&rfr_iscdi=true |