Post-capture vibration suppression of spacecraft via a bio-inspired isolation system
•A bio-inspired isolation system is proposed to suppress the micro-vibrations of a free-floating spacecraft.•Periodic and impulsive forces are considered to simulate the vibration sources on-board satellite.•The present isolator has been demonstrated to be superior to the traditional isolator by abo...
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Veröffentlicht in: | Mechanical systems and signal processing 2018-05, Vol.105, p.214-240 |
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creator | Dai, Honghua Jing, Xingjian Wang, Yu Yue, Xiaokui Yuan, Jianping |
description | •A bio-inspired isolation system is proposed to suppress the micro-vibrations of a free-floating spacecraft.•Periodic and impulsive forces are considered to simulate the vibration sources on-board satellite.•The present isolator has been demonstrated to be superior to the traditional isolator by about 10% in terms of acceleration amplitudes.•The isolation performance with nonlinear damping shows a much better performance.
Inspired by the smooth motions of a running kangaroo, a bio-inspired quadrilateral shape (BIQS) structure is proposed to suppress the vibrations of a free-floating spacecraft subject to periodic or impulsive forces, which may be encountered during on-orbit servicing missions. In particular, the BIQS structure is installed between the satellite platform and the capture mechanism. The dynamical model of the BIQS isolation system, i.e. a BIQS structure connecting the platform and the capture mechanism at each side, is established by Lagrange’s equations to simulate the post-capture dynamical responses. The BIQS system suffering an impulsive force is dealt with by means of a modified version of Lagrange’s equations. Furthermore, the classical harmonic balance method is used to solve the nonlinear dynamical system subject to periodic forces, while for the case under impulsive forces the numerical integration method is adopted. Due to the weightless environment in space, the present BIQS system is essentially an under-constrained dynamical system with one of its natural frequencies being identical to zero. The effects of system parameters, such as the number of layers in BIQS, stiffness, assembly angle, rod length, damping coefficient, masses of satellite platform and capture mechanism, on the isolation performance of the present system are thoroughly investigated. In addition, comparisons between the isolation performances of the presently proposed BIQS isolator and the conventional spring-mass-damper (SMD) isolator are conducted to demonstrate the advantages of the present isolator. Numerical simulations show that the BIQS system has a much better performance than the SMD system under either periodic or impulsive forces. Overall, the present BIQS isolator offers a highly efficient passive way for vibration suppressions of free-floating spacecraft. |
doi_str_mv | 10.1016/j.ymssp.2017.12.015 |
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Inspired by the smooth motions of a running kangaroo, a bio-inspired quadrilateral shape (BIQS) structure is proposed to suppress the vibrations of a free-floating spacecraft subject to periodic or impulsive forces, which may be encountered during on-orbit servicing missions. In particular, the BIQS structure is installed between the satellite platform and the capture mechanism. The dynamical model of the BIQS isolation system, i.e. a BIQS structure connecting the platform and the capture mechanism at each side, is established by Lagrange’s equations to simulate the post-capture dynamical responses. The BIQS system suffering an impulsive force is dealt with by means of a modified version of Lagrange’s equations. Furthermore, the classical harmonic balance method is used to solve the nonlinear dynamical system subject to periodic forces, while for the case under impulsive forces the numerical integration method is adopted. Due to the weightless environment in space, the present BIQS system is essentially an under-constrained dynamical system with one of its natural frequencies being identical to zero. The effects of system parameters, such as the number of layers in BIQS, stiffness, assembly angle, rod length, damping coefficient, masses of satellite platform and capture mechanism, on the isolation performance of the present system are thoroughly investigated. In addition, comparisons between the isolation performances of the presently proposed BIQS isolator and the conventional spring-mass-damper (SMD) isolator are conducted to demonstrate the advantages of the present isolator. Numerical simulations show that the BIQS system has a much better performance than the SMD system under either periodic or impulsive forces. Overall, the present BIQS isolator offers a highly efficient passive way for vibration suppressions of free-floating spacecraft.</description><identifier>ISSN: 0888-3270</identifier><identifier>EISSN: 1096-1216</identifier><identifier>DOI: 10.1016/j.ymssp.2017.12.015</identifier><language>eng</language><publisher>Berlin: Elsevier Ltd</publisher><subject>Bio-inspired ; Computer simulation ; Dynamical systems ; Euler-Lagrange equation ; Floating structures ; Harmonic balance method ; Impulsive force ; Lagrange multiplier ; Mathematical models ; Missions ; Nonlinear damping ; Numerical analysis ; Numerical integration ; On-orbit capture ; Spacecraft ; Spacecraft recovery ; Stiffness ; Studies ; Under-constrained system ; Vibration ; Vibration control ; Vibration isolation</subject><ispartof>Mechanical systems and signal processing, 2018-05, Vol.105, p.214-240</ispartof><rights>2017 Elsevier Ltd</rights><rights>Copyright Elsevier BV May 15, 2018</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c331t-d95301a012586df81adb7a09d9492b8026543ef4b76d695af33a239faf8f770f3</citedby><cites>FETCH-LOGICAL-c331t-d95301a012586df81adb7a09d9492b8026543ef4b76d695af33a239faf8f770f3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0888327017306507$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids></links><search><creatorcontrib>Dai, Honghua</creatorcontrib><creatorcontrib>Jing, Xingjian</creatorcontrib><creatorcontrib>Wang, Yu</creatorcontrib><creatorcontrib>Yue, Xiaokui</creatorcontrib><creatorcontrib>Yuan, Jianping</creatorcontrib><title>Post-capture vibration suppression of spacecraft via a bio-inspired isolation system</title><title>Mechanical systems and signal processing</title><description>•A bio-inspired isolation system is proposed to suppress the micro-vibrations of a free-floating spacecraft.•Periodic and impulsive forces are considered to simulate the vibration sources on-board satellite.•The present isolator has been demonstrated to be superior to the traditional isolator by about 10% in terms of acceleration amplitudes.•The isolation performance with nonlinear damping shows a much better performance.
Inspired by the smooth motions of a running kangaroo, a bio-inspired quadrilateral shape (BIQS) structure is proposed to suppress the vibrations of a free-floating spacecraft subject to periodic or impulsive forces, which may be encountered during on-orbit servicing missions. In particular, the BIQS structure is installed between the satellite platform and the capture mechanism. The dynamical model of the BIQS isolation system, i.e. a BIQS structure connecting the platform and the capture mechanism at each side, is established by Lagrange’s equations to simulate the post-capture dynamical responses. The BIQS system suffering an impulsive force is dealt with by means of a modified version of Lagrange’s equations. Furthermore, the classical harmonic balance method is used to solve the nonlinear dynamical system subject to periodic forces, while for the case under impulsive forces the numerical integration method is adopted. Due to the weightless environment in space, the present BIQS system is essentially an under-constrained dynamical system with one of its natural frequencies being identical to zero. The effects of system parameters, such as the number of layers in BIQS, stiffness, assembly angle, rod length, damping coefficient, masses of satellite platform and capture mechanism, on the isolation performance of the present system are thoroughly investigated. In addition, comparisons between the isolation performances of the presently proposed BIQS isolator and the conventional spring-mass-damper (SMD) isolator are conducted to demonstrate the advantages of the present isolator. Numerical simulations show that the BIQS system has a much better performance than the SMD system under either periodic or impulsive forces. Overall, the present BIQS isolator offers a highly efficient passive way for vibration suppressions of free-floating spacecraft.</description><subject>Bio-inspired</subject><subject>Computer simulation</subject><subject>Dynamical systems</subject><subject>Euler-Lagrange equation</subject><subject>Floating structures</subject><subject>Harmonic balance method</subject><subject>Impulsive force</subject><subject>Lagrange multiplier</subject><subject>Mathematical models</subject><subject>Missions</subject><subject>Nonlinear damping</subject><subject>Numerical analysis</subject><subject>Numerical integration</subject><subject>On-orbit capture</subject><subject>Spacecraft</subject><subject>Spacecraft recovery</subject><subject>Stiffness</subject><subject>Studies</subject><subject>Under-constrained system</subject><subject>Vibration</subject><subject>Vibration control</subject><subject>Vibration isolation</subject><issn>0888-3270</issn><issn>1096-1216</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2018</creationdate><recordtype>article</recordtype><recordid>eNp9kD1PwzAQhi0EEqXwC1giMSec7cSJBwZU8SVVgqHMlhPbkqM2Nr6kUv89Ke3MdDe8z53eh5B7CgUFKh774rBDjAUDWheUFUCrC7KgIEVOGRWXZAFN0-Sc1XBNbhB7AJAliAXZfAUc807HcUo22_s26dGHIcMpxmQRj3twGUbd2S5pN84Znems9SH3A0afrMk8hu0ZO-Bod7fkyukt2rvzXJLv15fN6j1ff759rJ7Xecc5HXMjKw5UA2VVI4xrqDZtrUEaWUrWNsBEVXLryrYWRshKO84149Jp17i6BseX5OF0N6bwM1kcVR-mNMwv1WyCl8BKCXOKn1JdCojJOhWT3-l0UBTUUZ_q1Z--I1QrytSsb6aeTpSdC-y9TQo7b4fOmrlyNyoT_L_8L5mZesQ</recordid><startdate>20180515</startdate><enddate>20180515</enddate><creator>Dai, Honghua</creator><creator>Jing, Xingjian</creator><creator>Wang, Yu</creator><creator>Yue, Xiaokui</creator><creator>Yuan, Jianping</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><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></search><sort><creationdate>20180515</creationdate><title>Post-capture vibration suppression of spacecraft via a bio-inspired isolation system</title><author>Dai, Honghua ; Jing, Xingjian ; Wang, Yu ; Yue, Xiaokui ; Yuan, Jianping</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c331t-d95301a012586df81adb7a09d9492b8026543ef4b76d695af33a239faf8f770f3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2018</creationdate><topic>Bio-inspired</topic><topic>Computer simulation</topic><topic>Dynamical systems</topic><topic>Euler-Lagrange equation</topic><topic>Floating structures</topic><topic>Harmonic balance method</topic><topic>Impulsive force</topic><topic>Lagrange multiplier</topic><topic>Mathematical models</topic><topic>Missions</topic><topic>Nonlinear damping</topic><topic>Numerical analysis</topic><topic>Numerical integration</topic><topic>On-orbit capture</topic><topic>Spacecraft</topic><topic>Spacecraft recovery</topic><topic>Stiffness</topic><topic>Studies</topic><topic>Under-constrained system</topic><topic>Vibration</topic><topic>Vibration control</topic><topic>Vibration isolation</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Dai, Honghua</creatorcontrib><creatorcontrib>Jing, Xingjian</creatorcontrib><creatorcontrib>Wang, Yu</creatorcontrib><creatorcontrib>Yue, Xiaokui</creatorcontrib><creatorcontrib>Yuan, Jianping</creatorcontrib><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><jtitle>Mechanical systems and signal processing</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Dai, Honghua</au><au>Jing, Xingjian</au><au>Wang, Yu</au><au>Yue, Xiaokui</au><au>Yuan, Jianping</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Post-capture vibration suppression of spacecraft via a bio-inspired isolation system</atitle><jtitle>Mechanical systems and signal processing</jtitle><date>2018-05-15</date><risdate>2018</risdate><volume>105</volume><spage>214</spage><epage>240</epage><pages>214-240</pages><issn>0888-3270</issn><eissn>1096-1216</eissn><abstract>•A bio-inspired isolation system is proposed to suppress the micro-vibrations of a free-floating spacecraft.•Periodic and impulsive forces are considered to simulate the vibration sources on-board satellite.•The present isolator has been demonstrated to be superior to the traditional isolator by about 10% in terms of acceleration amplitudes.•The isolation performance with nonlinear damping shows a much better performance.
Inspired by the smooth motions of a running kangaroo, a bio-inspired quadrilateral shape (BIQS) structure is proposed to suppress the vibrations of a free-floating spacecraft subject to periodic or impulsive forces, which may be encountered during on-orbit servicing missions. In particular, the BIQS structure is installed between the satellite platform and the capture mechanism. The dynamical model of the BIQS isolation system, i.e. a BIQS structure connecting the platform and the capture mechanism at each side, is established by Lagrange’s equations to simulate the post-capture dynamical responses. The BIQS system suffering an impulsive force is dealt with by means of a modified version of Lagrange’s equations. Furthermore, the classical harmonic balance method is used to solve the nonlinear dynamical system subject to periodic forces, while for the case under impulsive forces the numerical integration method is adopted. Due to the weightless environment in space, the present BIQS system is essentially an under-constrained dynamical system with one of its natural frequencies being identical to zero. The effects of system parameters, such as the number of layers in BIQS, stiffness, assembly angle, rod length, damping coefficient, masses of satellite platform and capture mechanism, on the isolation performance of the present system are thoroughly investigated. In addition, comparisons between the isolation performances of the presently proposed BIQS isolator and the conventional spring-mass-damper (SMD) isolator are conducted to demonstrate the advantages of the present isolator. Numerical simulations show that the BIQS system has a much better performance than the SMD system under either periodic or impulsive forces. Overall, the present BIQS isolator offers a highly efficient passive way for vibration suppressions of free-floating spacecraft.</abstract><cop>Berlin</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.ymssp.2017.12.015</doi><tpages>27</tpages></addata></record> |
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subjects | Bio-inspired Computer simulation Dynamical systems Euler-Lagrange equation Floating structures Harmonic balance method Impulsive force Lagrange multiplier Mathematical models Missions Nonlinear damping Numerical analysis Numerical integration On-orbit capture Spacecraft Spacecraft recovery Stiffness Studies Under-constrained system Vibration Vibration control Vibration isolation |
title | Post-capture vibration suppression of spacecraft via a bio-inspired isolation system |
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