Attitude Dynamics of Small Magnetic Axisymmetric Satellites in Near-Equatorial Low Earth Orbits/Very Low Earth Orbits
This study deals with the attitude motion of small magnetic axisymmetric satellites in near-equatorial circular low Earth orbits/very low Earth orbits subjected to the joint action of the environmental torques, namely, aerodynamic, gravitational, and magnetic. It is shown that if the satellite has o...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2024-12, Vol.47 (12), p.2544-2559 |
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| container_issue | 12 |
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| container_title | Journal of guidance, control, and dynamics |
| container_volume | 47 |
| creator | Sizov, Dmitry A. Aslanov, Vladimir S. |
| description | This study deals with the attitude motion of small magnetic axisymmetric satellites in near-equatorial circular low Earth orbits/very low Earth orbits subjected to the joint action of the environmental torques, namely, aerodynamic, gravitational, and magnetic. It is shown that if the satellite has only a longitudinal component of the intrinsic magnetic moment, it is convenient to separate the attitude motion into the unperturbed motion and the perturbations from the nonpotential components of the considered torques. The bifurcation analysis of the critical points of the unperturbed dynamic potential demonstrates the influence of the main system parameters on their existence and stability and provides an intuitive understanding of the possible regimes of attitude motion. Numerical simulations show that, in addition to regular attitude motion of the considered satellites, chaotic regimes are also possible. |
| doi_str_mv | 10.2514/1.G008393 |
| format | Article |
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It is shown that if the satellite has only a longitudinal component of the intrinsic magnetic moment, it is convenient to separate the attitude motion into the unperturbed motion and the perturbations from the nonpotential components of the considered torques. The bifurcation analysis of the critical points of the unperturbed dynamic potential demonstrates the influence of the main system parameters on their existence and stability and provides an intuitive understanding of the possible regimes of attitude motion. Numerical simulations show that, in addition to regular attitude motion of the considered satellites, chaotic regimes are also possible.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G008393</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Bifurcations ; Chaos theory ; Critical point ; Earth motion ; Inertia ; Integrals ; Low earth orbits ; Magnetic fields ; Magnetic moments ; Motion stability ; Orbits ; Satellites ; Torque</subject><ispartof>Journal of guidance, control, and dynamics, 2024-12, Vol.47 (12), p.2544-2559</ispartof><rights>Copyright © 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. 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 © 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 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-a178t-cee75cdcc29d97039ee550f02447631c2ebdd48635c425f37ba9da4ef3b6dde73</cites><orcidid>0000-0003-4065-137X ; 0000-0001-9077-8120</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>Sizov, Dmitry A.</creatorcontrib><creatorcontrib>Aslanov, Vladimir S.</creatorcontrib><title>Attitude Dynamics of Small Magnetic Axisymmetric Satellites in Near-Equatorial Low Earth Orbits/Very Low Earth Orbits</title><title>Journal of guidance, control, and dynamics</title><description>This study deals with the attitude motion of small magnetic axisymmetric satellites in near-equatorial circular low Earth orbits/very low Earth orbits subjected to the joint action of the environmental torques, namely, aerodynamic, gravitational, and magnetic. 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Numerical simulations show that, in addition to regular attitude motion of the considered satellites, chaotic regimes are also possible.</description><subject>Bifurcations</subject><subject>Chaos theory</subject><subject>Critical point</subject><subject>Earth motion</subject><subject>Inertia</subject><subject>Integrals</subject><subject>Low earth orbits</subject><subject>Magnetic fields</subject><subject>Magnetic moments</subject><subject>Motion stability</subject><subject>Orbits</subject><subject>Satellites</subject><subject>Torque</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><recordid>eNpl0M9LwzAUB_AgCs7pwf8gIAgeuiVN0rTHMecUpjtMvZY0edWM_tiSFO1_b2UDD54e7_Hh--CL0DUlk1hQPqWTJSEpy9gJGlHBWMTSlJ-iEZGMRoJk5BxdeL8lhLKEyhHqZiHY0BnA932jaqs9bku8qVVV4Wf10UCwGs--re_rGoIblo0KUFU2gMe2wS-gXLTYdyq0zqoKr9ovvFAufOK1K2zw03dw_b_rJTorVeXh6jjH6O1h8Tp_jFbr5dN8tooUlWmINIAU2mgdZyaThGUAQpCSxJzLhFEdQ2EMTxMmNI9FyWShMqM4lKxIjAHJxujmkLtz7b4DH_Jt27lmeJkzyhjnRCbxoO4OSrvWewdlvnO2Vq7PKcl_W81pfmx1sLcHq6xSf2n_4Q-ZsXZO</recordid><startdate>202412</startdate><enddate>202412</enddate><creator>Sizov, Dmitry A.</creator><creator>Aslanov, Vladimir S.</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><orcidid>https://orcid.org/0000-0003-4065-137X</orcidid><orcidid>https://orcid.org/0000-0001-9077-8120</orcidid></search><sort><creationdate>202412</creationdate><title>Attitude Dynamics of Small Magnetic Axisymmetric Satellites in Near-Equatorial Low Earth Orbits/Very Low Earth Orbits</title><author>Sizov, Dmitry A. ; Aslanov, Vladimir S.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a178t-cee75cdcc29d97039ee550f02447631c2ebdd48635c425f37ba9da4ef3b6dde73</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Bifurcations</topic><topic>Chaos theory</topic><topic>Critical point</topic><topic>Earth motion</topic><topic>Inertia</topic><topic>Integrals</topic><topic>Low earth orbits</topic><topic>Magnetic fields</topic><topic>Magnetic moments</topic><topic>Motion stability</topic><topic>Orbits</topic><topic>Satellites</topic><topic>Torque</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Sizov, Dmitry A.</creatorcontrib><creatorcontrib>Aslanov, Vladimir S.</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>Sizov, Dmitry A.</au><au>Aslanov, Vladimir S.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Attitude Dynamics of Small Magnetic Axisymmetric Satellites in Near-Equatorial Low Earth Orbits/Very Low Earth Orbits</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2024-12</date><risdate>2024</risdate><volume>47</volume><issue>12</issue><spage>2544</spage><epage>2559</epage><pages>2544-2559</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>This study deals with the attitude motion of small magnetic axisymmetric satellites in near-equatorial circular low Earth orbits/very low Earth orbits subjected to the joint action of the environmental torques, namely, aerodynamic, gravitational, and magnetic. 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| ispartof | Journal of guidance, control, and dynamics, 2024-12, Vol.47 (12), p.2544-2559 |
| issn | 0731-5090 1533-3884 |
| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Bifurcations Chaos theory Critical point Earth motion Inertia Integrals Low earth orbits Magnetic fields Magnetic moments Motion stability Orbits Satellites Torque |
| title | Attitude Dynamics of Small Magnetic Axisymmetric Satellites in Near-Equatorial Low Earth Orbits/Very Low Earth Orbits |
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