Sensorless Operation of a Permanent-Magnet Generator for Aircraft
This paper considers the operation and control of a brushless AC prototype embedded aircraft generator that has been designed for use as an alternative to the emergency run air turbine. To meet the wide operating speed requirements, the generator utilizes a hybrid rotor construction comprising perma...
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| Veröffentlicht in: | IEEE transactions on industry applications 2008-01, Vol.44 (1), p.101-107 |
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| container_title | IEEE transactions on industry applications |
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| creator | Burrow, S.G. Mellor, P.H. Churn, P. Sawata, T. Holme, M. |
| description | This paper considers the operation and control of a brushless AC prototype embedded aircraft generator that has been designed for use as an alternative to the emergency run air turbine. To meet the wide operating speed requirements, the generator utilizes a hybrid rotor construction comprising permanent magnet and variable reluctance sections. The constant current source characteristics of the design are exploited to derive the phase information required by the AC vector controller, thus avoiding the use of a shaft-mounted rotor position sensor. The methodology behind the controller operation is presented together with test results taken from a prototype generator system, and this is contrast with the results taken from the conventionally controlled machine with resolver position feedback. |
| doi_str_mv | 10.1109/TIA.2007.912756 |
| format | Article |
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To meet the wide operating speed requirements, the generator utilizes a hybrid rotor construction comprising permanent magnet and variable reluctance sections. The constant current source characteristics of the design are exploited to derive the phase information required by the AC vector controller, thus avoiding the use of a shaft-mounted rotor position sensor. The methodology behind the controller operation is presented together with test results taken from a prototype generator system, and this is contrast with the results taken from the conventionally controlled machine with resolver position feedback.</description><identifier>ISSN: 0093-9994</identifier><identifier>EISSN: 1939-9367</identifier><identifier>DOI: 10.1109/TIA.2007.912756</identifier><identifier>CODEN: ITIACR</identifier><language>eng</language><publisher>New York: IEEE</publisher><subject>AC generators ; Aerospace control ; Air conditioning ; Aircraft ; Aircraft industry ; Aircraft manufacture ; Control systems ; Embedded aircraft generation ; Emergency procedures ; Generators ; hybrid permanent-magnet (PM)/variable reluctance machines ; Magnetic variables control ; Permanent magnet motors ; power factor control ; Prototypes ; Rotors ; Sensorless control ; Turbines</subject><ispartof>IEEE transactions on industry applications, 2008-01, Vol.44 (1), p.101-107</ispartof><rights>Copyright The Institute of Electrical and Electronics Engineers, Inc. (IEEE) 2008</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c320t-67a4a00068e8ab2eb65ef2e96ae853f15eb988b059748699a6b24f959038e1ee3</citedby><cites>FETCH-LOGICAL-c320t-67a4a00068e8ab2eb65ef2e96ae853f15eb988b059748699a6b24f959038e1ee3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/4439762$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,780,784,796,4021,27921,27922,27923,54756</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/4439762$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Burrow, S.G.</creatorcontrib><creatorcontrib>Mellor, P.H.</creatorcontrib><creatorcontrib>Churn, P.</creatorcontrib><creatorcontrib>Sawata, T.</creatorcontrib><creatorcontrib>Holme, M.</creatorcontrib><title>Sensorless Operation of a Permanent-Magnet Generator for Aircraft</title><title>IEEE transactions on industry applications</title><addtitle>TIA</addtitle><description>This paper considers the operation and control of a brushless AC prototype embedded aircraft generator that has been designed for use as an alternative to the emergency run air turbine. To meet the wide operating speed requirements, the generator utilizes a hybrid rotor construction comprising permanent magnet and variable reluctance sections. The constant current source characteristics of the design are exploited to derive the phase information required by the AC vector controller, thus avoiding the use of a shaft-mounted rotor position sensor. The methodology behind the controller operation is presented together with test results taken from a prototype generator system, and this is contrast with the results taken from the conventionally controlled machine with resolver position feedback.</description><subject>AC generators</subject><subject>Aerospace control</subject><subject>Air conditioning</subject><subject>Aircraft</subject><subject>Aircraft industry</subject><subject>Aircraft manufacture</subject><subject>Control systems</subject><subject>Embedded aircraft generation</subject><subject>Emergency procedures</subject><subject>Generators</subject><subject>hybrid permanent-magnet (PM)/variable reluctance machines</subject><subject>Magnetic variables control</subject><subject>Permanent magnet motors</subject><subject>power factor control</subject><subject>Prototypes</subject><subject>Rotors</subject><subject>Sensorless control</subject><subject>Turbines</subject><issn>0093-9994</issn><issn>1939-9367</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2008</creationdate><recordtype>article</recordtype><sourceid>RIE</sourceid><recordid>eNpdkEtLw0AUhQdRsD7WLtwEN67S3nlm7rIUrYVKBet6mIQ7kpImdSZd-O9Nibhwcbmb7xwOH2N3HKacA862q_lUABRT5KLQ5oxNOErMUZrinE0AUOaIqC7ZVUo7AK40VxM2f6c2dbGhlLLNgaLv667NupD57I3i3rfU9vmr_2ypz5bUnoAuZmG4eR2r6EN_wy6CbxLd_v5r9vH8tF285OvNcrWYr_NKCuhzU3jlAcBYsr4UVBpNQRAaT1bLwDWVaG0JGgtlDaI3pVABNYK0xInkNXscew-x-zpS6t2-ThU1zbCxOyZnCw0GjJED-fCP3HXH2A7jnDWCcyGFGqDZCFWxSylScIdY7338dhzcSagbhLqTUDcKHRL3Y6Imoj9aKYmFEfIHvQdv4A</recordid><startdate>200801</startdate><enddate>200801</enddate><creator>Burrow, S.G.</creator><creator>Mellor, P.H.</creator><creator>Churn, P.</creator><creator>Sawata, T.</creator><creator>Holme, M.</creator><general>IEEE</general><general>The Institute of Electrical and Electronics Engineers, Inc. (IEEE)</general><scope>97E</scope><scope>RIA</scope><scope>RIE</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7SC</scope><scope>7SP</scope><scope>8FD</scope><scope>JQ2</scope><scope>L7M</scope><scope>L~C</scope><scope>L~D</scope><scope>F28</scope><scope>FR3</scope><scope>H8D</scope></search><sort><creationdate>200801</creationdate><title>Sensorless Operation of a Permanent-Magnet Generator for Aircraft</title><author>Burrow, S.G. ; Mellor, P.H. ; Churn, P. ; Sawata, T. ; Holme, M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c320t-67a4a00068e8ab2eb65ef2e96ae853f15eb988b059748699a6b24f959038e1ee3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2008</creationdate><topic>AC generators</topic><topic>Aerospace control</topic><topic>Air conditioning</topic><topic>Aircraft</topic><topic>Aircraft industry</topic><topic>Aircraft manufacture</topic><topic>Control systems</topic><topic>Embedded aircraft generation</topic><topic>Emergency procedures</topic><topic>Generators</topic><topic>hybrid permanent-magnet (PM)/variable reluctance machines</topic><topic>Magnetic variables control</topic><topic>Permanent magnet motors</topic><topic>power factor control</topic><topic>Prototypes</topic><topic>Rotors</topic><topic>Sensorless control</topic><topic>Turbines</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Burrow, S.G.</creatorcontrib><creatorcontrib>Mellor, P.H.</creatorcontrib><creatorcontrib>Churn, P.</creatorcontrib><creatorcontrib>Sawata, T.</creatorcontrib><creatorcontrib>Holme, M.</creatorcontrib><collection>IEEE All-Society Periodicals Package (ASPP) 2005-present</collection><collection>IEEE All-Society Periodicals Package (ASPP) 1998-Present</collection><collection>IEEE Electronic Library (IEL)</collection><collection>CrossRef</collection><collection>Computer and Information Systems Abstracts</collection><collection>Electronics & Communications Abstracts</collection><collection>Technology Research 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><collection>ANTE: Abstracts in New Technology & Engineering</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><jtitle>IEEE transactions on industry applications</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Burrow, S.G.</au><au>Mellor, P.H.</au><au>Churn, P.</au><au>Sawata, T.</au><au>Holme, M.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Sensorless Operation of a Permanent-Magnet Generator for Aircraft</atitle><jtitle>IEEE transactions on industry applications</jtitle><stitle>TIA</stitle><date>2008-01</date><risdate>2008</risdate><volume>44</volume><issue>1</issue><spage>101</spage><epage>107</epage><pages>101-107</pages><issn>0093-9994</issn><eissn>1939-9367</eissn><coden>ITIACR</coden><abstract>This paper considers the operation and control of a brushless AC prototype embedded aircraft generator that has been designed for use as an alternative to the emergency run air turbine. To meet the wide operating speed requirements, the generator utilizes a hybrid rotor construction comprising permanent magnet and variable reluctance sections. The constant current source characteristics of the design are exploited to derive the phase information required by the AC vector controller, thus avoiding the use of a shaft-mounted rotor position sensor. The methodology behind the controller operation is presented together with test results taken from a prototype generator system, and this is contrast with the results taken from the conventionally controlled machine with resolver position feedback.</abstract><cop>New York</cop><pub>IEEE</pub><doi>10.1109/TIA.2007.912756</doi><tpages>7</tpages></addata></record> |
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| ispartof | IEEE transactions on industry applications, 2008-01, Vol.44 (1), p.101-107 |
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| language | eng |
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| source | IEEE Electronic Library (IEL) |
| subjects | AC generators Aerospace control Air conditioning Aircraft Aircraft industry Aircraft manufacture Control systems Embedded aircraft generation Emergency procedures Generators hybrid permanent-magnet (PM)/variable reluctance machines Magnetic variables control Permanent magnet motors power factor control Prototypes Rotors Sensorless control Turbines |
| title | Sensorless Operation of a Permanent-Magnet Generator for Aircraft |
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