Nonlinear vibration analysis of a novel moving mass flight vehicle
In view of the control authority and configuration, a novel configuration of moving mass with large mass ratio is proposed and its nonlinear dynamics is investigated. The coupling dynamic equations between angle of attack and deflection of moving mass are established. An analysis of these equations...
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| Veröffentlicht in: | Nonlinear dynamics 2017-10, Vol.90 (1), p.733-748 |
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| container_title | Nonlinear dynamics |
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| creator | Li, Jianqing Gao, Changsheng Jing, Wuxing Fan, Yidi |
| description | In view of the control authority and configuration, a novel configuration of moving mass with large mass ratio is proposed and its nonlinear dynamics is investigated. The coupling dynamic equations between angle of attack and deflection of moving mass are established. An analysis of these equations indicates that the moving mass with large mass ratio will result in dynamic equations having nonlinearities and the occurrence of internal resonances in such system. Multiple-scale method is used in the analysis of the primary resonances of the external excitation and internal resonances. The steady-state solutions and the effects of different parameters of moving mass on the frequency response have been investigated. Numerical results show that the proposed system is of hardening spring characteristic when excitation frequency is near to different natural frequencies. The mass ratio and the relative position also lead to the occurrence of a jump phenomenon and multi-valued regions. The reasonable design for parameters of the moving mass system can ensure stability and high performance of flight vehicle. |
| doi_str_mv | 10.1007/s11071-017-3691-y |
| format | Article |
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The coupling dynamic equations between angle of attack and deflection of moving mass are established. An analysis of these equations indicates that the moving mass with large mass ratio will result in dynamic equations having nonlinearities and the occurrence of internal resonances in such system. Multiple-scale method is used in the analysis of the primary resonances of the external excitation and internal resonances. The steady-state solutions and the effects of different parameters of moving mass on the frequency response have been investigated. Numerical results show that the proposed system is of hardening spring characteristic when excitation frequency is near to different natural frequencies. The mass ratio and the relative position also lead to the occurrence of a jump phenomenon and multi-valued regions. The reasonable design for parameters of the moving mass system can ensure stability and high performance of flight vehicle.</description><identifier>ISSN: 0924-090X</identifier><identifier>EISSN: 1573-269X</identifier><identifier>DOI: 10.1007/s11071-017-3691-y</identifier><language>eng</language><publisher>Dordrecht: Springer Netherlands</publisher><subject>Angle of attack ; Automotive Engineering ; Classical Mechanics ; Configurations ; Control ; Design parameters ; Dynamical Systems ; Engineering ; Excitation ; Flight vehicles ; Frequency response ; Mechanical Engineering ; Nonlinear analysis ; Nonlinear dynamics ; Original Paper ; Resonant frequencies ; Vibration ; Vibration analysis</subject><ispartof>Nonlinear dynamics, 2017-10, Vol.90 (1), p.733-748</ispartof><rights>Springer Science+Business Media B.V. 2017</rights><rights>Copyright Springer Science & Business Media 2017</rights><rights>Nonlinear Dynamics is a copyright of Springer, (2017). All Rights Reserved.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c344t-59dfe1a389b57a4f3b77386b99c4e3d45c9ac60ae984846e88e58b4d86f2d6e43</citedby><cites>FETCH-LOGICAL-c344t-59dfe1a389b57a4f3b77386b99c4e3d45c9ac60ae984846e88e58b4d86f2d6e43</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s11071-017-3691-y$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s11071-017-3691-y$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27901,27902,41464,42533,51294</link.rule.ids></links><search><creatorcontrib>Li, Jianqing</creatorcontrib><creatorcontrib>Gao, Changsheng</creatorcontrib><creatorcontrib>Jing, Wuxing</creatorcontrib><creatorcontrib>Fan, Yidi</creatorcontrib><title>Nonlinear vibration analysis of a novel moving mass flight vehicle</title><title>Nonlinear dynamics</title><addtitle>Nonlinear Dyn</addtitle><description>In view of the control authority and configuration, a novel configuration of moving mass with large mass ratio is proposed and its nonlinear dynamics is investigated. The coupling dynamic equations between angle of attack and deflection of moving mass are established. An analysis of these equations indicates that the moving mass with large mass ratio will result in dynamic equations having nonlinearities and the occurrence of internal resonances in such system. Multiple-scale method is used in the analysis of the primary resonances of the external excitation and internal resonances. The steady-state solutions and the effects of different parameters of moving mass on the frequency response have been investigated. Numerical results show that the proposed system is of hardening spring characteristic when excitation frequency is near to different natural frequencies. The mass ratio and the relative position also lead to the occurrence of a jump phenomenon and multi-valued regions. The reasonable design for parameters of the moving mass system can ensure stability and high performance of flight vehicle.</description><subject>Angle of attack</subject><subject>Automotive Engineering</subject><subject>Classical Mechanics</subject><subject>Configurations</subject><subject>Control</subject><subject>Design parameters</subject><subject>Dynamical Systems</subject><subject>Engineering</subject><subject>Excitation</subject><subject>Flight vehicles</subject><subject>Frequency response</subject><subject>Mechanical Engineering</subject><subject>Nonlinear analysis</subject><subject>Nonlinear dynamics</subject><subject>Original Paper</subject><subject>Resonant frequencies</subject><subject>Vibration</subject><subject>Vibration analysis</subject><issn>0924-090X</issn><issn>1573-269X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2017</creationdate><recordtype>article</recordtype><sourceid>BENPR</sourceid><recordid>eNp9kDtPwzAURi0EEqXwA9gsMRuuH4ntESpeUgULSN0sJ3FaV2lc7DRS_j2pwsAC013O-XR1ELqmcEsB5F2iFCQlQCXhuaZkOEEzmklOWK5Xp2gGmgkCGlbn6CKlLQBwBmqGHt5C2_jW2Yh7X0Tb-dBi29pmSD7hUGOL29C7Bu9C79s13tmUcN349abDvdv4snGX6Ky2TXJXP3eOPp8ePxYvZPn-_Lq4X5KSC9GRTFe1o5YrXWTSipoXUnKVF1qXwvFKZKW2ZQ7WaSWUyJ1SLlOFqFResyp3gs_RzbS7j-Hr4FJntuEQx1eTYSzTIhNcsv8oOjKKCylhpOhElTGkFF1t9tHvbBwMBXMMaqagZgxqjkHNMDpsctLItmsXfy3_KX0D68N4Nw</recordid><startdate>20171001</startdate><enddate>20171001</enddate><creator>Li, Jianqing</creator><creator>Gao, Changsheng</creator><creator>Jing, Wuxing</creator><creator>Fan, Yidi</creator><general>Springer Netherlands</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M7S</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20171001</creationdate><title>Nonlinear vibration analysis of a novel moving mass flight vehicle</title><author>Li, Jianqing ; Gao, Changsheng ; Jing, Wuxing ; Fan, Yidi</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c344t-59dfe1a389b57a4f3b77386b99c4e3d45c9ac60ae984846e88e58b4d86f2d6e43</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2017</creationdate><topic>Angle of attack</topic><topic>Automotive Engineering</topic><topic>Classical Mechanics</topic><topic>Configurations</topic><topic>Control</topic><topic>Design parameters</topic><topic>Dynamical Systems</topic><topic>Engineering</topic><topic>Excitation</topic><topic>Flight vehicles</topic><topic>Frequency response</topic><topic>Mechanical Engineering</topic><topic>Nonlinear analysis</topic><topic>Nonlinear dynamics</topic><topic>Original Paper</topic><topic>Resonant frequencies</topic><topic>Vibration</topic><topic>Vibration analysis</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Li, Jianqing</creatorcontrib><creatorcontrib>Gao, Changsheng</creatorcontrib><creatorcontrib>Jing, Wuxing</creatorcontrib><creatorcontrib>Fan, Yidi</creatorcontrib><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central Korea</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering Collection</collection><jtitle>Nonlinear dynamics</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Li, Jianqing</au><au>Gao, Changsheng</au><au>Jing, Wuxing</au><au>Fan, Yidi</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Nonlinear vibration analysis of a novel moving mass flight vehicle</atitle><jtitle>Nonlinear dynamics</jtitle><stitle>Nonlinear Dyn</stitle><date>2017-10-01</date><risdate>2017</risdate><volume>90</volume><issue>1</issue><spage>733</spage><epage>748</epage><pages>733-748</pages><issn>0924-090X</issn><eissn>1573-269X</eissn><abstract>In view of the control authority and configuration, a novel configuration of moving mass with large mass ratio is proposed and its nonlinear dynamics is investigated. The coupling dynamic equations between angle of attack and deflection of moving mass are established. An analysis of these equations indicates that the moving mass with large mass ratio will result in dynamic equations having nonlinearities and the occurrence of internal resonances in such system. Multiple-scale method is used in the analysis of the primary resonances of the external excitation and internal resonances. The steady-state solutions and the effects of different parameters of moving mass on the frequency response have been investigated. Numerical results show that the proposed system is of hardening spring characteristic when excitation frequency is near to different natural frequencies. The mass ratio and the relative position also lead to the occurrence of a jump phenomenon and multi-valued regions. The reasonable design for parameters of the moving mass system can ensure stability and high performance of flight vehicle.</abstract><cop>Dordrecht</cop><pub>Springer Netherlands</pub><doi>10.1007/s11071-017-3691-y</doi><tpages>16</tpages></addata></record> |
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| subjects | Angle of attack Automotive Engineering Classical Mechanics Configurations Control Design parameters Dynamical Systems Engineering Excitation Flight vehicles Frequency response Mechanical Engineering Nonlinear analysis Nonlinear dynamics Original Paper Resonant frequencies Vibration Vibration analysis |
| title | Nonlinear vibration analysis of a novel moving mass flight vehicle |
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