Autonomous Navigation Using X-Ray Pulsars and Multirate Processing
In this paper, autonomous pulsar-based spacecraft navigation is formulated in terms of a single nonlinear filter. The observability and the positioning accuracy of a spacecraft traveling at known constant velocity are analyzed to build insights into the general navigation problem. A variation of the...
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| Veröffentlicht in: | Journal of guidance, control, and dynamics control, and dynamics, 2017-09, Vol.40 (9), p.2237-2249 |
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| container_title | Journal of guidance, control, and dynamics |
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| creator | Chen, Po-Ting Speyer, Jason L Bayard, David S Majid, Walid A |
| description | In this paper, autonomous pulsar-based spacecraft navigation is formulated in terms of a single nonlinear filter. The observability and the positioning accuracy of a spacecraft traveling at known constant velocity are analyzed to build insights into the general navigation problem. A variation of the extended Kalman filter is developed and implemented to track Poisson pulsar measurements collected by an orbiting spacecraft. This filter leverages multirate structure to more efficiently process pulsar measurements. An alternative formulation using quadrature is studied, and its performance is compared to the typical phase approach. Simulation results for an orbiter mission and a deep-space mission are presented to show the accuracy of pulsar-based navigation in space. |
| doi_str_mv | 10.2514/1.G002705 |
| format | Article |
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The observability and the positioning accuracy of a spacecraft traveling at known constant velocity are analyzed to build insights into the general navigation problem. A variation of the extended Kalman filter is developed and implemented to track Poisson pulsar measurements collected by an orbiting spacecraft. This filter leverages multirate structure to more efficiently process pulsar measurements. An alternative formulation using quadrature is studied, and its performance is compared to the typical phase approach. Simulation results for an orbiter mission and a deep-space mission are presented to show the accuracy of pulsar-based navigation in space.</description><identifier>ISSN: 0731-5090</identifier><identifier>EISSN: 1533-3884</identifier><identifier>DOI: 10.2514/1.G002705</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Accuracy ; Autonomous navigation ; Deep space ; Extended Kalman filter ; Laboratories ; Navigation systems ; Noise ; Nonlinear filters ; Observability (systems) ; Pulsars ; Quadratures ; Radio communications ; Solar system ; Space missions ; Space shuttle ; Spacecraft ; Spacecraft tracking ; Sun ; Velocity</subject><ispartof>Journal of guidance, control, and dynamics, 2017-09, Vol.40 (9), p.2237-2249</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><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c313t-5f878f909cf17f2c031b8e4503387d5240dc22fc0933073c1a73b2eece86a0833</citedby><cites>FETCH-LOGICAL-c313t-5f878f909cf17f2c031b8e4503387d5240dc22fc0933073c1a73b2eece86a0833</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27924,27925</link.rule.ids></links><search><creatorcontrib>Chen, Po-Ting</creatorcontrib><creatorcontrib>Speyer, Jason L</creatorcontrib><creatorcontrib>Bayard, David S</creatorcontrib><creatorcontrib>Majid, Walid A</creatorcontrib><title>Autonomous Navigation Using X-Ray Pulsars and Multirate Processing</title><title>Journal of guidance, control, and dynamics</title><description>In this paper, autonomous pulsar-based spacecraft navigation is formulated in terms of a single nonlinear filter. 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Simulation results for an orbiter mission and a deep-space mission are presented to show the accuracy of pulsar-based navigation in space.</description><subject>Accuracy</subject><subject>Autonomous navigation</subject><subject>Deep space</subject><subject>Extended Kalman filter</subject><subject>Laboratories</subject><subject>Navigation systems</subject><subject>Noise</subject><subject>Nonlinear filters</subject><subject>Observability (systems)</subject><subject>Pulsars</subject><subject>Quadratures</subject><subject>Radio communications</subject><subject>Solar system</subject><subject>Space missions</subject><subject>Space shuttle</subject><subject>Spacecraft</subject><subject>Spacecraft tracking</subject><subject>Sun</subject><subject>Velocity</subject><issn>0731-5090</issn><issn>1533-3884</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><recordid>eNp90MFKAzEQgOEgCtbqwTdY8ORh60wmaZJjLVqFqkUseFvSNFu2tJua7Ap9e7e0Z09z-ZgZfsZuEQZconjAwQSAK5BnrIeSKCetxTnrgSLMJRi4ZFcprQGQhqh67HHUNqEO29Cm7N3-VivbVKHO5qmqV9l3_mn32azdJBtTZutl9tZumiraxmezGJxPB3bNLkq7Sf7mNPts_vz0NX7Jpx-T1_FomjtCanJZaqVLA8aVqErugHChvZBApNVScgFLx3npwBB13zq0ihbce-f10IIm6rO7495dDD-tT02xDm2su5MFF0YoIw2q_xQapZUU0HX5T2mjBEppoFP3R-ViSCn6stjFamvjvkAoDrkLLE656Q84T25c</recordid><startdate>20170901</startdate><enddate>20170901</enddate><creator>Chen, Po-Ting</creator><creator>Speyer, Jason L</creator><creator>Bayard, David S</creator><creator>Majid, Walid A</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>20170901</creationdate><title>Autonomous Navigation Using X-Ray Pulsars and Multirate Processing</title><author>Chen, Po-Ting ; Speyer, Jason L ; Bayard, David S ; Majid, Walid A</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c313t-5f878f909cf17f2c031b8e4503387d5240dc22fc0933073c1a73b2eece86a0833</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Accuracy</topic><topic>Autonomous navigation</topic><topic>Deep space</topic><topic>Extended Kalman filter</topic><topic>Laboratories</topic><topic>Navigation systems</topic><topic>Noise</topic><topic>Nonlinear filters</topic><topic>Observability (systems)</topic><topic>Pulsars</topic><topic>Quadratures</topic><topic>Radio communications</topic><topic>Solar system</topic><topic>Space missions</topic><topic>Space shuttle</topic><topic>Spacecraft</topic><topic>Spacecraft tracking</topic><topic>Sun</topic><topic>Velocity</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Chen, Po-Ting</creatorcontrib><creatorcontrib>Speyer, Jason L</creatorcontrib><creatorcontrib>Bayard, David S</creatorcontrib><creatorcontrib>Majid, Walid A</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, Po-Ting</au><au>Speyer, Jason L</au><au>Bayard, David S</au><au>Majid, Walid A</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Autonomous Navigation Using X-Ray Pulsars and Multirate Processing</atitle><jtitle>Journal of guidance, control, and dynamics</jtitle><date>2017-09-01</date><risdate>2017</risdate><volume>40</volume><issue>9</issue><spage>2237</spage><epage>2249</epage><pages>2237-2249</pages><issn>0731-5090</issn><eissn>1533-3884</eissn><abstract>In this paper, autonomous pulsar-based spacecraft navigation is formulated in terms of a single nonlinear filter. 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| language | eng |
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| source | Alma/SFX Local Collection |
| subjects | Accuracy Autonomous navigation Deep space Extended Kalman filter Laboratories Navigation systems Noise Nonlinear filters Observability (systems) Pulsars Quadratures Radio communications Solar system Space missions Space shuttle Spacecraft Spacecraft tracking Sun Velocity |
| title | Autonomous Navigation Using X-Ray Pulsars and Multirate Processing |
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