Precise Solar Radiation Pressure Models for Small-Body Orbiters: Applications to OSIRIS-REx Spacecraft
This paper presents a framework for the precise representation of solar radiation pressure effects on spacecraft orbiting around small bodies. It uses a Fourier-series expansion to model the solar radiation force that is imparted on the spacecraft. A set of dominant Fourier coefficients that account...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2017-07, Vol.40 (7), p.1638-1650 |
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| container_title | Journal of guidance, control, and dynamics |
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| creator | Hesar, Siamak G Scheeres, Daniel J McMahon, Jay W |
| description | This paper presents a framework for the precise representation of solar radiation pressure effects on spacecraft orbiting around small bodies. It uses a Fourier-series expansion to model the solar radiation force that is imparted on the spacecraft. A set of dominant Fourier coefficients that account for a majority of the solar radiation pressure effect and its uncertainty is identified. Analytical solutions are derived to shed light on the secular effects of solar radiation pressure on the orbit of spacecraft around small bodies. As an example application, this framework is implemented for the precise estimation of solar radiation pressure effects on the Origins, Spectral Interpretation, Resource Identification, Security, Regolith Explorer spacecraft in orbit about asteroid (101955) Bennu. A set of error analyses and covariance studies are carried out for this spacecraft to evaluate the expected level of estimation precision that is feasible for the dominant Fourier coefficients. |
| doi_str_mv | 10.2514/1.G002323 |
| format | Article |
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It uses a Fourier-series expansion to model the solar radiation force that is imparted on the spacecraft. A set of dominant Fourier coefficients that account for a majority of the solar radiation pressure effect and its uncertainty is identified. Analytical solutions are derived to shed light on the secular effects of solar radiation pressure on the orbit of spacecraft around small bodies. As an example application, this framework is implemented for the precise estimation of solar radiation pressure effects on the Origins, Spectral Interpretation, Resource Identification, Security, Regolith Explorer spacecraft in orbit about asteroid (101955) Bennu. A set of error analyses and covariance studies are carried out for this spacecraft to evaluate the expected level of estimation precision that is feasible for the dominant Fourier coefficients.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G002323</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Aerospace engineering ; Apollo asteroids ; Asteroid missions ; Asteroids ; Coefficients ; Covariance ; Error analysis ; Exact solutions ; Feasibility studies ; Fourier analysis ; Fourier series ; Global positioning systems ; GPS ; Mathematical models ; Methods ; Numerical analysis ; Orbits ; Origins ; Pressure effects ; Radiation ; Radiation pressure ; Regolith ; Satellites ; Security ; Series expansion ; Solar radiation ; Spacecraft ; Spacecraft orbits ; Spectra ; Uncertainty ; Uncertainty analysis</subject><ispartof>Journal of guidance, control, and dynamics, 2017-07, Vol.40 (7), p.1638-1650</ispartof><rights>Copyright © 2017 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 ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.</rights><rights>Copyright © 2017 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 ISSN 0731-5090 (print) or 1533-3884 (online) to initiate your request. 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It uses a Fourier-series expansion to model the solar radiation force that is imparted on the spacecraft. A set of dominant Fourier coefficients that account for a majority of the solar radiation pressure effect and its uncertainty is identified. Analytical solutions are derived to shed light on the secular effects of solar radiation pressure on the orbit of spacecraft around small bodies. As an example application, this framework is implemented for the precise estimation of solar radiation pressure effects on the Origins, Spectral Interpretation, Resource Identification, Security, Regolith Explorer spacecraft in orbit about asteroid (101955) Bennu. A set of error analyses and covariance studies are carried out for this spacecraft to evaluate the expected level of estimation precision that is feasible for the dominant Fourier coefficients.</description><subject>Aerospace engineering</subject><subject>Apollo asteroids</subject><subject>Asteroid missions</subject><subject>Asteroids</subject><subject>Coefficients</subject><subject>Covariance</subject><subject>Error analysis</subject><subject>Exact solutions</subject><subject>Feasibility studies</subject><subject>Fourier analysis</subject><subject>Fourier series</subject><subject>Global positioning systems</subject><subject>GPS</subject><subject>Mathematical models</subject><subject>Methods</subject><subject>Numerical analysis</subject><subject>Orbits</subject><subject>Origins</subject><subject>Pressure effects</subject><subject>Radiation</subject><subject>Radiation pressure</subject><subject>Regolith</subject><subject>Satellites</subject><subject>Security</subject><subject>Series expansion</subject><subject>Solar radiation</subject><subject>Spacecraft</subject><subject>Spacecraft orbits</subject><subject>Spectra</subject><subject>Uncertainty</subject><subject>Uncertainty analysis</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp9kcFLwzAYxYMoOKcH_4OAJw-dSb6mTbzNMedgMln1XL6mCXR0S006cP-90-2804PH7713eITcczYSkqdPfDRjTICACzLgEiABpdJLMmA58EQyza7JTYxrxjhkPB8Q9xGsaaKlhW8x0BXWDfaN39KDH-MuWPrua9tG6nygxQbbNnnx9Z4uQ9X0NsRnOu66tjH_oUh7T5fFfDUvktX0hxYdGmsCuv6WXDlso7076ZB8vU4_J2_JYjmbT8aLxACHPlFSadSOZ7wSWS3AopUpCGdyCVVlESGtoFbArKtAMuUEaIsaZVbVKLCGIXk49nbBf-9s7Mu134XtYbIUqU6lElqpcxTXTAPPpZRnKaUFKJFLfqAej5QJPsZgXdmFZoNhX3JW_l1S8vJ0CfwCT0N7yQ</recordid><startdate>20170701</startdate><enddate>20170701</enddate><creator>Hesar, Siamak G</creator><creator>Scheeres, Daniel J</creator><creator>McMahon, Jay W</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>20170701</creationdate><title>Precise Solar Radiation Pressure Models for Small-Body Orbiters: Applications to OSIRIS-REx Spacecraft</title><author>Hesar, Siamak G ; Scheeres, Daniel J ; McMahon, Jay W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c313t-8589a9f161b26d23eae5432fc753bbeaa34b3d830efb3508f239ea9a56bda2ad3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Aerospace engineering</topic><topic>Apollo asteroids</topic><topic>Asteroid missions</topic><topic>Asteroids</topic><topic>Coefficients</topic><topic>Covariance</topic><topic>Error analysis</topic><topic>Exact solutions</topic><topic>Feasibility studies</topic><topic>Fourier analysis</topic><topic>Fourier series</topic><topic>Global positioning systems</topic><topic>GPS</topic><topic>Mathematical models</topic><topic>Methods</topic><topic>Numerical analysis</topic><topic>Orbits</topic><topic>Origins</topic><topic>Pressure effects</topic><topic>Radiation</topic><topic>Radiation pressure</topic><topic>Regolith</topic><topic>Satellites</topic><topic>Security</topic><topic>Series expansion</topic><topic>Solar radiation</topic><topic>Spacecraft</topic><topic>Spacecraft orbits</topic><topic>Spectra</topic><topic>Uncertainty</topic><topic>Uncertainty analysis</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Hesar, Siamak G</creatorcontrib><creatorcontrib>Scheeres, Daniel J</creatorcontrib><creatorcontrib>McMahon, Jay W</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>Hesar, Siamak G</au><au>Scheeres, Daniel J</au><au>McMahon, Jay W</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Precise Solar Radiation Pressure Models for Small-Body Orbiters: Applications to OSIRIS-REx Spacecraft</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2017-07-01</date><risdate>2017</risdate><volume>40</volume><issue>7</issue><spage>1638</spage><epage>1650</epage><pages>1638-1650</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>This paper presents a framework for the precise representation of solar radiation pressure effects on spacecraft orbiting around small bodies. 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| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Aerospace engineering Apollo asteroids Asteroid missions Asteroids Coefficients Covariance Error analysis Exact solutions Feasibility studies Fourier analysis Fourier series Global positioning systems GPS Mathematical models Methods Numerical analysis Orbits Origins Pressure effects Radiation Radiation pressure Regolith Satellites Security Series expansion Solar radiation Spacecraft Spacecraft orbits Spectra Uncertainty Uncertainty analysis |
| title | Precise Solar Radiation Pressure Models for Small-Body Orbiters: Applications to OSIRIS-REx Spacecraft |
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