Stable Orbiting Around Small Moons Using J2-Perturbed Elliptic Restricted Problem
Confirmed small-body missions Martian Moons eXploration (MMX) and Hera are set to explore Martian moons and the binary asteroid Didymos’s moon Dimorphos, respectively. Orbital dynamics around these small moons differ substantially from those around previously visited targets. Simplified models, such...
Gespeichert in:
Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2024-07, Vol.47 (7), p.1327-1340 |
---|---|
Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | 1340 |
---|---|
container_issue | 7 |
container_start_page | 1327 |
container_title | Journal of guidance, control, and dynamics |
container_volume | 47 |
creator | Chen, Hongru Hou, Xiyun Bando, Mai |
description | Confirmed small-body missions Martian Moons eXploration (MMX) and Hera are set to explore Martian moons and the binary asteroid Didymos’s moon Dimorphos, respectively. Orbital dynamics around these small moons differ substantially from those around previously visited targets. Simplified models, such as the circular-restricted three-body problem, cannot yield accurate predictions for orbits and their stability in real-world operations. To be specific, the orbit of the small moon and its vicinity are significantly perturbed by the oblateness of the planet and their relative positions. Realistic control constraints and the unstable 3:1 resonance of retrograde orbits further complicate orbit maintenance around a small moon. Therefore, minimizing the dynamical perturbation on baseline orbits resulting from model mismatches is crucial. This paper introduces the J2-ER3BP+GH model dedicated to describing the orbital dynamics around the small moon. It incorporates the [Formula: see text] perturbation of the planet on the elliptic-restricted three-body problem and can accommodate a nonspherical gravity field of the moon. Bounded orbits can still be identified without much effort in this sophisticated model. Baseline orbits around Phobos and Dimorphos from the J2-ER3BP+GH model become much easier to maintain, as verified in the high-fidelity dynamic and control environments. |
doi_str_mv | 10.2514/1.G008001 |
format | Article |
fullrecord | <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_3072008972</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>3072008972</sourcerecordid><originalsourceid>FETCH-LOGICAL-c226t-9ea49775a6c92b194d2a0d74d420eeaba8d32be5dc721d9af7692d881fc6ca2f3</originalsourceid><addsrcrecordid>eNotkMFOAjEQhhujiYgefIMmnjwsttPd7fZICKIGA4qcm27bNUuWLbbdA29vCZwm-efLP5MPoUdKJlDQ_IVOFoRUhNArNKIFYxmrqvwajQhnNCuIILfoLoRdAlhJ-Qh9baKqO4tXvm5j2__iqXdDb_Bmr7oOfzrXB7wNp8UHZGvr4-Bra_C869pDbDX-tiH6VseUrb1LTft7dNOoLtiHyxyj7ev8Z_aWLVeL99l0mWmAMmbCqlxwXqhSC6ipyA0oYnhuciDWqlpVhkFtC6M5UCNUw0sBpqpoo0utoGFj9HTuPXj3N6Q35M4Nvk8nJSMckgXBIVHPZ0p7F4K3jTz4dq_8UVIiT8YklRdj7B_iD10O</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>3072008972</pqid></control><display><type>article</type><title>Stable Orbiting Around Small Moons Using J2-Perturbed Elliptic Restricted Problem</title><source>Alma/SFX Local Collection</source><creator>Chen, Hongru ; Hou, Xiyun ; Bando, Mai</creator><creatorcontrib>Chen, Hongru ; Hou, Xiyun ; Bando, Mai</creatorcontrib><description>Confirmed small-body missions Martian Moons eXploration (MMX) and Hera are set to explore Martian moons and the binary asteroid Didymos’s moon Dimorphos, respectively. Orbital dynamics around these small moons differ substantially from those around previously visited targets. Simplified models, such as the circular-restricted three-body problem, cannot yield accurate predictions for orbits and their stability in real-world operations. To be specific, the orbit of the small moon and its vicinity are significantly perturbed by the oblateness of the planet and their relative positions. Realistic control constraints and the unstable 3:1 resonance of retrograde orbits further complicate orbit maintenance around a small moon. Therefore, minimizing the dynamical perturbation on baseline orbits resulting from model mismatches is crucial. This paper introduces the J2-ER3BP+GH model dedicated to describing the orbital dynamics around the small moon. It incorporates the [Formula: see text] perturbation of the planet on the elliptic-restricted three-body problem and can accommodate a nonspherical gravity field of the moon. Bounded orbits can still be identified without much effort in this sophisticated model. Baseline orbits around Phobos and Dimorphos from the J2-ER3BP+GH model become much easier to maintain, as verified in the high-fidelity dynamic and control environments.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G008001</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Gravitational fields ; Mars missions ; Mars satellites ; Moon ; Orbit perturbation ; Orbital mechanics ; Orbital resonances (celestial mechanics) ; Orbital stability ; Orbits ; Phobos ; Retrograde orbits ; Three body problem</subject><ispartof>Journal of guidance, control, and dynamics, 2024-07, Vol.47 (7), p.1327-1340</ispartof><rights>Copyright © 2024 by Hongru Chen, Xiyun Hou, and Mai Bando. 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 ISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><cites>FETCH-LOGICAL-c226t-9ea49775a6c92b194d2a0d74d420eeaba8d32be5dc721d9af7692d881fc6ca2f3</cites><orcidid>0000-0001-9453-6962 ; 0000-0002-8970-7592</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,776,780,27903,27904</link.rule.ids></links><search><creatorcontrib>Chen, Hongru</creatorcontrib><creatorcontrib>Hou, Xiyun</creatorcontrib><creatorcontrib>Bando, Mai</creatorcontrib><title>Stable Orbiting Around Small Moons Using J2-Perturbed Elliptic Restricted Problem</title><title>Journal of guidance, control, and dynamics</title><description>Confirmed small-body missions Martian Moons eXploration (MMX) and Hera are set to explore Martian moons and the binary asteroid Didymos’s moon Dimorphos, respectively. Orbital dynamics around these small moons differ substantially from those around previously visited targets. Simplified models, such as the circular-restricted three-body problem, cannot yield accurate predictions for orbits and their stability in real-world operations. To be specific, the orbit of the small moon and its vicinity are significantly perturbed by the oblateness of the planet and their relative positions. Realistic control constraints and the unstable 3:1 resonance of retrograde orbits further complicate orbit maintenance around a small moon. Therefore, minimizing the dynamical perturbation on baseline orbits resulting from model mismatches is crucial. This paper introduces the J2-ER3BP+GH model dedicated to describing the orbital dynamics around the small moon. It incorporates the [Formula: see text] perturbation of the planet on the elliptic-restricted three-body problem and can accommodate a nonspherical gravity field of the moon. Bounded orbits can still be identified without much effort in this sophisticated model. Baseline orbits around Phobos and Dimorphos from the J2-ER3BP+GH model become much easier to maintain, as verified in the high-fidelity dynamic and control environments.</description><subject>Gravitational fields</subject><subject>Mars missions</subject><subject>Mars satellites</subject><subject>Moon</subject><subject>Orbit perturbation</subject><subject>Orbital mechanics</subject><subject>Orbital resonances (celestial mechanics)</subject><subject>Orbital stability</subject><subject>Orbits</subject><subject>Phobos</subject><subject>Retrograde orbits</subject><subject>Three body problem</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2024</creationdate><recordtype>article</recordtype><recordid>eNotkMFOAjEQhhujiYgefIMmnjwsttPd7fZICKIGA4qcm27bNUuWLbbdA29vCZwm-efLP5MPoUdKJlDQ_IVOFoRUhNArNKIFYxmrqvwajQhnNCuIILfoLoRdAlhJ-Qh9baKqO4tXvm5j2__iqXdDb_Bmr7oOfzrXB7wNp8UHZGvr4-Bra_C869pDbDX-tiH6VseUrb1LTft7dNOoLtiHyxyj7ev8Z_aWLVeL99l0mWmAMmbCqlxwXqhSC6ipyA0oYnhuciDWqlpVhkFtC6M5UCNUw0sBpqpoo0utoGFj9HTuPXj3N6Q35M4Nvk8nJSMckgXBIVHPZ0p7F4K3jTz4dq_8UVIiT8YklRdj7B_iD10O</recordid><startdate>202407</startdate><enddate>202407</enddate><creator>Chen, Hongru</creator><creator>Hou, Xiyun</creator><creator>Bando, Mai</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/0000-0001-9453-6962</orcidid><orcidid>https://orcid.org/0000-0002-8970-7592</orcidid></search><sort><creationdate>202407</creationdate><title>Stable Orbiting Around Small Moons Using J2-Perturbed Elliptic Restricted Problem</title><author>Chen, Hongru ; Hou, Xiyun ; Bando, Mai</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c226t-9ea49775a6c92b194d2a0d74d420eeaba8d32be5dc721d9af7692d881fc6ca2f3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2024</creationdate><topic>Gravitational fields</topic><topic>Mars missions</topic><topic>Mars satellites</topic><topic>Moon</topic><topic>Orbit perturbation</topic><topic>Orbital mechanics</topic><topic>Orbital resonances (celestial mechanics)</topic><topic>Orbital stability</topic><topic>Orbits</topic><topic>Phobos</topic><topic>Retrograde orbits</topic><topic>Three body problem</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Hongru</creatorcontrib><creatorcontrib>Hou, Xiyun</creatorcontrib><creatorcontrib>Bando, Mai</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>Chen, Hongru</au><au>Hou, Xiyun</au><au>Bando, Mai</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Stable Orbiting Around Small Moons Using J2-Perturbed Elliptic Restricted Problem</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2024-07</date><risdate>2024</risdate><volume>47</volume><issue>7</issue><spage>1327</spage><epage>1340</epage><pages>1327-1340</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>Confirmed small-body missions Martian Moons eXploration (MMX) and Hera are set to explore Martian moons and the binary asteroid Didymos’s moon Dimorphos, respectively. Orbital dynamics around these small moons differ substantially from those around previously visited targets. Simplified models, such as the circular-restricted three-body problem, cannot yield accurate predictions for orbits and their stability in real-world operations. To be specific, the orbit of the small moon and its vicinity are significantly perturbed by the oblateness of the planet and their relative positions. Realistic control constraints and the unstable 3:1 resonance of retrograde orbits further complicate orbit maintenance around a small moon. Therefore, minimizing the dynamical perturbation on baseline orbits resulting from model mismatches is crucial. This paper introduces the J2-ER3BP+GH model dedicated to describing the orbital dynamics around the small moon. It incorporates the [Formula: see text] perturbation of the planet on the elliptic-restricted three-body problem and can accommodate a nonspherical gravity field of the moon. Bounded orbits can still be identified without much effort in this sophisticated model. Baseline orbits around Phobos and Dimorphos from the J2-ER3BP+GH model become much easier to maintain, as verified in the high-fidelity dynamic and control environments.</abstract><cop>Reston</cop><pub>American Institute of Aeronautics and Astronautics</pub><doi>10.2514/1.G008001</doi><tpages>14</tpages><orcidid>https://orcid.org/0000-0001-9453-6962</orcidid><orcidid>https://orcid.org/0000-0002-8970-7592</orcidid><oa>free_for_read</oa></addata></record> |
fulltext | fulltext |
identifier | ISSN: 0731-5090 |
ispartof | Journal of guidance, control, and dynamics, 2024-07, Vol.47 (7), p.1327-1340 |
issn | 0731-5090 1533-3884 |
language | eng |
recordid | cdi_proquest_journals_3072008972 |
source | Alma/SFX Local Collection |
subjects | Gravitational fields Mars missions Mars satellites Moon Orbit perturbation Orbital mechanics Orbital resonances (celestial mechanics) Orbital stability Orbits Phobos Retrograde orbits Three body problem |
title | Stable Orbiting Around Small Moons Using J2-Perturbed Elliptic Restricted Problem |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-22T22%3A03%3A56IST&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=Stable%20Orbiting%20Around%20Small%20Moons%20Using%20J2-Perturbed%20Elliptic%20Restricted%20Problem&rft.jtitle=Journal%20of%20guidance,%20control,%20and%20dynamics&rft.au=Chen,%20Hongru&rft.date=2024-07&rft.volume=47&rft.issue=7&rft.spage=1327&rft.epage=1340&rft.pages=1327-1340&rft.issn=0731-5090&rft.eissn=1533-3884&rft_id=info:doi/10.2514/1.G008001&rft_dat=%3Cproquest_cross%3E3072008972%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=3072008972&rft_id=info:pmid/&rfr_iscdi=true |