Active control on the vibration of flexible satellites --Variable structure control method and experiment
The flexible satellites with large solar panels require strong robustness of attitude control systems, so that good dynamic properties and high precision of attitude orientation and adjustment can be maintained even under the action of various uncertainties. As solar panels have been placed on some...
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Veröffentlicht in: | 中国科学通报:英文版 1995 (23), p.2007-2011 |
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container_end_page | 2011 |
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container_issue | 23 |
container_start_page | 2007 |
container_title | 中国科学通报:英文版 |
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creator | 周军 李季苏 牟小刚 汪春涛 |
description | The flexible satellites with large solar panels require strong robustness of attitude control systems, so that good dynamic properties and high precision of attitude orientation and adjustment can be maintained even under the action of various uncertainties. As solar panels have been placed on some new type of our satellites, it is necessary to study the control schemes and the corresponding experiments from the viewpoint of engineering. |
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As solar panels have been placed on some new type of our satellites, it is necessary to study the control schemes and the corresponding experiments from the viewpoint of engineering.</description><identifier>ISSN: 2095-9273</identifier><language>eng</language><subject>control ; experimental ; flexible ; satellites ; setup ; structure ; variable ; VSC</subject><ispartof>中国科学通报:英文版, 1995 (23), p.2007-2011</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Uhttp://image.cqvip.com/vip1000/qk/86894X/86894X.jpg</thumbnail><link.rule.ids>314,776,780,4010</link.rule.ids></links><search><creatorcontrib>周军 李季苏 牟小刚 汪春涛</creatorcontrib><title>Active control on the vibration of flexible satellites --Variable structure control method and experiment</title><title>中国科学通报:英文版</title><addtitle>Chinese Science Bulletin</addtitle><description>The flexible satellites with large solar panels require strong robustness of attitude control systems, so that good dynamic properties and high precision of attitude orientation and adjustment can be maintained even under the action of various uncertainties. As solar panels have been placed on some new type of our satellites, it is necessary to study the control schemes and the corresponding experiments from the viewpoint of engineering.</description><subject>control</subject><subject>experimental</subject><subject>flexible</subject><subject>satellites</subject><subject>setup</subject><subject>structure</subject><subject>variable</subject><subject>VSC</subject><issn>2095-9273</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1995</creationdate><recordtype>article</recordtype><recordid>eNqNjsEKwjAQRHNQULT_sOA5kKaW2qOI4geIV4nt1q7ERJOt1L-3iODV0_CGxzAjMdWqzGWpi2wikhivSql0WeqlKqaC1hXTE6HyjoO34B1wi_CkczBMA_kGGos9nS1CNIzWEmMEKY8mkPm0HLqKu_AbuSG3vgbjasD-joFu6Hguxo2xEZNvzsRitz1s9rJqvbs8yF1O98E04XXKhoNaZ6s0z_6z3u1xSHc</recordid><startdate>1995</startdate><enddate>1995</enddate><creator>周军 李季苏 牟小刚 汪春涛</creator><scope>2RA</scope><scope>92L</scope><scope>CQIGP</scope><scope>~WA</scope></search><sort><creationdate>1995</creationdate><title>Active control on the vibration of flexible satellites --Variable structure control method and experiment</title><author>周军 李季苏 牟小刚 汪春涛</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-chongqing_primary_30012238153</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1995</creationdate><topic>control</topic><topic>experimental</topic><topic>flexible</topic><topic>satellites</topic><topic>setup</topic><topic>structure</topic><topic>variable</topic><topic>VSC</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>周军 李季苏 牟小刚 汪春涛</creatorcontrib><collection>中文科技期刊数据库</collection><collection>中文科技期刊数据库-CALIS站点</collection><collection>中文科技期刊数据库-7.0平台</collection><collection>中文科技期刊数据库- 镜像站点</collection><jtitle>中国科学通报:英文版</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>周军 李季苏 牟小刚 汪春涛</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Active control on the vibration of flexible satellites --Variable structure control method and experiment</atitle><jtitle>中国科学通报:英文版</jtitle><addtitle>Chinese Science Bulletin</addtitle><date>1995</date><risdate>1995</risdate><issue>23</issue><spage>2007</spage><epage>2011</epage><pages>2007-2011</pages><issn>2095-9273</issn><abstract>The flexible satellites with large solar panels require strong robustness of attitude control systems, so that good dynamic properties and high precision of attitude orientation and adjustment can be maintained even under the action of various uncertainties. As solar panels have been placed on some new type of our satellites, it is necessary to study the control schemes and the corresponding experiments from the viewpoint of engineering.</abstract></addata></record> |
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identifier | ISSN: 2095-9273 |
ispartof | 中国科学通报:英文版, 1995 (23), p.2007-2011 |
issn | 2095-9273 |
language | eng |
recordid | cdi_chongqing_primary_3001223815 |
source | Alma/SFX Local Collection |
subjects | control experimental flexible satellites setup structure variable VSC |
title | Active control on the vibration of flexible satellites --Variable structure control method and experiment |
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