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Error Modeling and Compensation of Circular Motion on a New Circumferential Drilling System
A new flexible circumferential drilling system is proposed to drill on the fuselage docking area. To analyze the influence of the circular motion error to the drilling accuracy, the nominal forward kinematic model is derived using Denavit-Hartenberg (D-H) method and this model is further developed t...
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Published in: | Mathematical problems in engineering 2015-01, Vol.2015 (2015), p.1-8 |
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container_title | Mathematical problems in engineering |
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creator | Han, Yong-Wei Fei, Shao-Hua Li, Yu-Chao Fang, Qiang Ke, Ying-Lin |
description | A new flexible circumferential drilling system is proposed to drill on the fuselage docking area. To analyze the influence of the circular motion error to the drilling accuracy, the nominal forward kinematic model is derived using Denavit-Hartenberg (D-H) method and this model is further developed to model the kinematic errors caused by circular positioning error and synchronization error using homogeneous transformation matrices (HTM). A laser tracker is utilized to measure the circular motion error of the two measurement points at both sides. A circular motion compensation experiment is implemented according to the calculated positioning error and synchronization error. Experimental results show that the positioning error and synchronization error were reduced by 65.0% and 58.8%, respectively, due to the adopted compensation, and therefore the circular motion accuracy is substantially improved. Finally, position errors of the two measurement points are analyzed to have little influence on the measurement result and the validity of the proposed compensation method is proved. |
doi_str_mv | 10.1155/2015/286796 |
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To analyze the influence of the circular motion error to the drilling accuracy, the nominal forward kinematic model is derived using Denavit-Hartenberg (D-H) method and this model is further developed to model the kinematic errors caused by circular positioning error and synchronization error using homogeneous transformation matrices (HTM). A laser tracker is utilized to measure the circular motion error of the two measurement points at both sides. A circular motion compensation experiment is implemented according to the calculated positioning error and synchronization error. Experimental results show that the positioning error and synchronization error were reduced by 65.0% and 58.8%, respectively, due to the adopted compensation, and therefore the circular motion accuracy is substantially improved. Finally, position errors of the two measurement points are analyzed to have little influence on the measurement result and the validity of the proposed compensation method is proved.</description><identifier>ISSN: 1024-123X</identifier><identifier>EISSN: 1563-5147</identifier><identifier>DOI: 10.1155/2015/286796</identifier><language>eng</language><publisher>Cairo, Egypt: Hindawi Publishing Corporation</publisher><subject>Accuracy ; Aerospace industry ; Aircraft ; Automation ; Circularity ; Compensation ; Coordinate transformations ; Drilling ; Error analysis ; Errors ; Kinematics ; Mathematical models ; Motion compensation ; Position errors ; Position measurement ; Synchronism ; Synchronization</subject><ispartof>Mathematical problems in engineering, 2015-01, Vol.2015 (2015), p.1-8</ispartof><rights>Copyright © 2015 Qiang Fang et al.</rights><rights>Copyright © 2015 Qiang Fang et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c389t-302d3fa43d241e4f3d7174d5eabadb3fdeef566e222254d46b57f440b7246a533</citedby><cites>FETCH-LOGICAL-c389t-302d3fa43d241e4f3d7174d5eabadb3fdeef566e222254d46b57f440b7246a533</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://www.proquest.com/docview/1721310286/fulltextPDF?pq-origsite=primo$$EPDF$$P50$$Gproquest$$Hfree_for_read</linktopdf><linktohtml>$$Uhttps://www.proquest.com/docview/1721310286?pq-origsite=primo$$EHTML$$P50$$Gproquest$$Hfree_for_read</linktohtml><link.rule.ids>314,776,780,25730,27900,27901,36988,36989,44565,75095</link.rule.ids></links><search><contributor>Chang, Qing</contributor><creatorcontrib>Han, Yong-Wei</creatorcontrib><creatorcontrib>Fei, Shao-Hua</creatorcontrib><creatorcontrib>Li, Yu-Chao</creatorcontrib><creatorcontrib>Fang, Qiang</creatorcontrib><creatorcontrib>Ke, Ying-Lin</creatorcontrib><title>Error Modeling and Compensation of Circular Motion on a New Circumferential Drilling System</title><title>Mathematical problems in engineering</title><description>A new flexible circumferential drilling system is proposed to drill on the fuselage docking area. To analyze the influence of the circular motion error to the drilling accuracy, the nominal forward kinematic model is derived using Denavit-Hartenberg (D-H) method and this model is further developed to model the kinematic errors caused by circular positioning error and synchronization error using homogeneous transformation matrices (HTM). A laser tracker is utilized to measure the circular motion error of the two measurement points at both sides. A circular motion compensation experiment is implemented according to the calculated positioning error and synchronization error. Experimental results show that the positioning error and synchronization error were reduced by 65.0% and 58.8%, respectively, due to the adopted compensation, and therefore the circular motion accuracy is substantially improved. Finally, position errors of the two measurement points are analyzed to have little influence on the measurement result and the validity of the proposed compensation method is proved.</description><subject>Accuracy</subject><subject>Aerospace industry</subject><subject>Aircraft</subject><subject>Automation</subject><subject>Circularity</subject><subject>Compensation</subject><subject>Coordinate transformations</subject><subject>Drilling</subject><subject>Error analysis</subject><subject>Errors</subject><subject>Kinematics</subject><subject>Mathematical models</subject><subject>Motion compensation</subject><subject>Position errors</subject><subject>Position measurement</subject><subject>Synchronism</subject><subject>Synchronization</subject><issn>1024-123X</issn><issn>1563-5147</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2015</creationdate><recordtype>article</recordtype><sourceid>PIMPY</sourceid><recordid>eNqF0E1LxDAQBuAiCq6rJ-9S8CJKtflse5S6fsCqBxUEDyVtJpqlTdakZdl_b9Z6EC_mkAyTh2F4o-gQpecIMXaBUxSunGcF34omiHGSMESz7VCnmCYIk9fdaM_7RZpixFA-id5mzlkX31sJrTbvsTAyLm23BONFr62JrYpL7ZqhFRs1tkws4gdYjR-dAgem16KNr5xuv6c8rX0P3X60o0Tr4eDnnUYv17Pn8jaZP97clZfzpCF50SckxZIoQYnEFAFVRGYoo5KBqIWsiZIAinEOOBxGJeU1yxSlaZ1hygUjZBqdjHOXzn4O4Puq076BthUG7OArlBUEY17keaDHf-jCDs6E7YLCiISYch7U2agaZ713oKql051w6wql1SboahN0NQYd9OmoP7SRYqX_wUcjhkBAiV84IzRs8AUBT4YO</recordid><startdate>20150101</startdate><enddate>20150101</enddate><creator>Han, Yong-Wei</creator><creator>Fei, Shao-Hua</creator><creator>Li, Yu-Chao</creator><creator>Fang, Qiang</creator><creator>Ke, Ying-Lin</creator><general>Hindawi Publishing Corporation</general><general>Hindawi Limited</general><scope>ADJCN</scope><scope>AHFXO</scope><scope>RHU</scope><scope>RHW</scope><scope>RHX</scope><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>ABUWG</scope><scope>AFKRA</scope><scope>ARAPS</scope><scope>AZQEC</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>CWDGH</scope><scope>DWQXO</scope><scope>FR3</scope><scope>GNUQQ</scope><scope>HCIFZ</scope><scope>JQ2</scope><scope>K7-</scope><scope>KR7</scope><scope>L6V</scope><scope>M7S</scope><scope>P5Z</scope><scope>P62</scope><scope>PHGZM</scope><scope>PHGZT</scope><scope>PIMPY</scope><scope>PKEHL</scope><scope>PQEST</scope><scope>PQGLB</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20150101</creationdate><title>Error Modeling and Compensation of Circular Motion on a New Circumferential Drilling System</title><author>Han, Yong-Wei ; 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To analyze the influence of the circular motion error to the drilling accuracy, the nominal forward kinematic model is derived using Denavit-Hartenberg (D-H) method and this model is further developed to model the kinematic errors caused by circular positioning error and synchronization error using homogeneous transformation matrices (HTM). A laser tracker is utilized to measure the circular motion error of the two measurement points at both sides. A circular motion compensation experiment is implemented according to the calculated positioning error and synchronization error. Experimental results show that the positioning error and synchronization error were reduced by 65.0% and 58.8%, respectively, due to the adopted compensation, and therefore the circular motion accuracy is substantially improved. Finally, position errors of the two measurement points are analyzed to have little influence on the measurement result and the validity of the proposed compensation method is proved.</abstract><cop>Cairo, Egypt</cop><pub>Hindawi Publishing Corporation</pub><doi>10.1155/2015/286796</doi><tpages>8</tpages><oa>free_for_read</oa></addata></record> |
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subjects | Accuracy Aerospace industry Aircraft Automation Circularity Compensation Coordinate transformations Drilling Error analysis Errors Kinematics Mathematical models Motion compensation Position errors Position measurement Synchronism Synchronization |
title | Error Modeling and Compensation of Circular Motion on a New Circumferential Drilling System |
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