Macroparticle launch velocity control in rail accelerators
The paper is devoted to the development of the method to increase the stability of the macroparticle launch velocity in the electromagnetic rail accelerators for the simulation of space debris. The method is based on the acceleration process control in the real time. The principle of the accelerator...
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| Veröffentlicht in: | IEEE transactions on magnetics 1997-01, Vol.33 (1), p.213-218 |
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| container_title | IEEE transactions on magnetics |
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| creator | Azanov, I.B. Alexandrov, V.A. Obydennikov, S.S. Tyutin, V.K. Khrustalev, M.M. Yudas, V.I. |
| description | The paper is devoted to the development of the method to increase the stability of the macroparticle launch velocity in the electromagnetic rail accelerators for the simulation of space debris. The method is based on the acceleration process control in the real time. The principle of the accelerator control is in varying the armature current and macroparticle acceleration with a circuit bypassing. The control algorithm with memory has been investigated. The acceleration process control reduces the effect of disturbances in accelerator parameters and initial conditions, as well as the effect of measurement errors upon the spread in launch velocities. The control algorithm efficiency is checked by numerical modeling of operation of the laboratory rail accelerator with plasma armature. |
| doi_str_mv | 10.1109/20.559957 |
| format | Article |
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The method is based on the acceleration process control in the real time. The principle of the accelerator control is in varying the armature current and macroparticle acceleration with a circuit bypassing. The control algorithm with memory has been investigated. The acceleration process control reduces the effect of disturbances in accelerator parameters and initial conditions, as well as the effect of measurement errors upon the spread in launch velocities. The control algorithm efficiency is checked by numerical modeling of operation of the laboratory rail accelerator with plasma armature.</description><identifier>ISSN: 0018-9464</identifier><identifier>EISSN: 1941-0069</identifier><identifier>DOI: 10.1109/20.559957</identifier><identifier>CODEN: IEMGAQ</identifier><language>eng</language><publisher>IEEE</publisher><subject>Acceleration ; Accelerometers ; Circuit simulation ; Circuit stability ; Electromagnetic launching ; Plasma accelerators ; Process control ; Rails ; Space debris ; Velocity control</subject><ispartof>IEEE transactions on magnetics, 1997-01, Vol.33 (1), p.213-218</ispartof><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c277t-c94e7f1ed28160f00b21ed175f0568ca0640e26d0d0adc56180e81f3d9e65b5e3</citedby></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://ieeexplore.ieee.org/document/559957$$EHTML$$P50$$Gieee$$H</linktohtml><link.rule.ids>314,780,784,796,27922,27923,54756</link.rule.ids><linktorsrc>$$Uhttps://ieeexplore.ieee.org/document/559957$$EView_record_in_IEEE$$FView_record_in_$$GIEEE</linktorsrc></links><search><creatorcontrib>Azanov, I.B.</creatorcontrib><creatorcontrib>Alexandrov, V.A.</creatorcontrib><creatorcontrib>Obydennikov, S.S.</creatorcontrib><creatorcontrib>Tyutin, V.K.</creatorcontrib><creatorcontrib>Khrustalev, M.M.</creatorcontrib><creatorcontrib>Yudas, V.I.</creatorcontrib><title>Macroparticle launch velocity control in rail accelerators</title><title>IEEE transactions on magnetics</title><addtitle>TMAG</addtitle><description>The paper is devoted to the development of the method to increase the stability of the macroparticle launch velocity in the electromagnetic rail accelerators for the simulation of space debris. The method is based on the acceleration process control in the real time. The principle of the accelerator control is in varying the armature current and macroparticle acceleration with a circuit bypassing. The control algorithm with memory has been investigated. The acceleration process control reduces the effect of disturbances in accelerator parameters and initial conditions, as well as the effect of measurement errors upon the spread in launch velocities. The control algorithm efficiency is checked by numerical modeling of operation of the laboratory rail accelerator with plasma armature.</description><subject>Acceleration</subject><subject>Accelerometers</subject><subject>Circuit simulation</subject><subject>Circuit stability</subject><subject>Electromagnetic launching</subject><subject>Plasma accelerators</subject><subject>Process control</subject><subject>Rails</subject><subject>Space debris</subject><subject>Velocity control</subject><issn>0018-9464</issn><issn>1941-0069</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1997</creationdate><recordtype>article</recordtype><recordid>eNo9kM1LxDAQxYMouK4evHrqSfDQdSZt0sSbLH7Bihc9h2w6xUi2WZOusP-9lS6ehsf8eLz3GLtEWCCCvuWwEEJr0RyxGeoaSwCpj9kMAFWpa1mfsrOcv0ZZC4QZu3u1LsWtTYN3gYpgd737LH4oROeHfeFiP6QYCt8XyfpQWOcoULJDTPmcnXQ2ZLo43Dn7eHx4Xz6Xq7enl-X9qnS8aYbS6ZqaDqnlCiV0AGs-CmxEB0IqZ0HWQFy20IJtnZCogBR2VatJirWgas6uJ99tit87yoPZ-DzGCLanuMuGq6pRlZIjeDOBY6OcE3Vmm_zGpr1BMH_rGA5mWmdkrybWE9E_d3j-AqtIXzg</recordid><startdate>199701</startdate><enddate>199701</enddate><creator>Azanov, I.B.</creator><creator>Alexandrov, V.A.</creator><creator>Obydennikov, S.S.</creator><creator>Tyutin, V.K.</creator><creator>Khrustalev, M.M.</creator><creator>Yudas, V.I.</creator><general>IEEE</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>8FD</scope><scope>L7M</scope></search><sort><creationdate>199701</creationdate><title>Macroparticle launch velocity control in rail accelerators</title><author>Azanov, I.B. ; Alexandrov, V.A. ; Obydennikov, S.S. ; Tyutin, V.K. ; Khrustalev, M.M. ; Yudas, V.I.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c277t-c94e7f1ed28160f00b21ed175f0568ca0640e26d0d0adc56180e81f3d9e65b5e3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1997</creationdate><topic>Acceleration</topic><topic>Accelerometers</topic><topic>Circuit simulation</topic><topic>Circuit stability</topic><topic>Electromagnetic launching</topic><topic>Plasma accelerators</topic><topic>Process control</topic><topic>Rails</topic><topic>Space debris</topic><topic>Velocity control</topic><toplevel>online_resources</toplevel><creatorcontrib>Azanov, I.B.</creatorcontrib><creatorcontrib>Alexandrov, V.A.</creatorcontrib><creatorcontrib>Obydennikov, S.S.</creatorcontrib><creatorcontrib>Tyutin, V.K.</creatorcontrib><creatorcontrib>Khrustalev, M.M.</creatorcontrib><creatorcontrib>Yudas, V.I.</creatorcontrib><collection>CrossRef</collection><collection>Electronics & Communications Abstracts</collection><collection>Technology Research Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>IEEE transactions on magnetics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Azanov, I.B.</au><au>Alexandrov, V.A.</au><au>Obydennikov, S.S.</au><au>Tyutin, V.K.</au><au>Khrustalev, M.M.</au><au>Yudas, V.I.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Macroparticle launch velocity control in rail accelerators</atitle><jtitle>IEEE transactions on magnetics</jtitle><stitle>TMAG</stitle><date>1997-01</date><risdate>1997</risdate><volume>33</volume><issue>1</issue><spage>213</spage><epage>218</epage><pages>213-218</pages><issn>0018-9464</issn><eissn>1941-0069</eissn><coden>IEMGAQ</coden><abstract>The paper is devoted to the development of the method to increase the stability of the macroparticle launch velocity in the electromagnetic rail accelerators for the simulation of space debris. The method is based on the acceleration process control in the real time. The principle of the accelerator control is in varying the armature current and macroparticle acceleration with a circuit bypassing. The control algorithm with memory has been investigated. The acceleration process control reduces the effect of disturbances in accelerator parameters and initial conditions, as well as the effect of measurement errors upon the spread in launch velocities. The control algorithm efficiency is checked by numerical modeling of operation of the laboratory rail accelerator with plasma armature.</abstract><pub>IEEE</pub><doi>10.1109/20.559957</doi><tpages>6</tpages></addata></record> |
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| ispartof | IEEE transactions on magnetics, 1997-01, Vol.33 (1), p.213-218 |
| issn | 0018-9464 1941-0069 |
| language | eng |
| recordid | cdi_proquest_miscellaneous_28378386 |
| source | IEEE Electronic Library (IEL) |
| subjects | Acceleration Accelerometers Circuit simulation Circuit stability Electromagnetic launching Plasma accelerators Process control Rails Space debris Velocity control |
| title | Macroparticle launch velocity control in rail accelerators |
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