Robust attitude control method of space interceptor
The invention provides a robust attitude control method of a space interceptor. The method includes the following steps: step 1, establishing an aircraft attitude model; and step 2, designing a robustnonlinear attitude stabilization controller. 本发明提供了一种空间拦截器鲁棒姿态控制方法,包括以下步骤:步骤1,建立飞行器姿态模型步骤2,设计鲁棒非线性姿态...
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creator | ZHOU CHENGBAO LI RUXIANG WANG GUOYOU JIN KAIWEN LU MINGKUI WANG KUI LI QICHANG LIANG DONGDONG BAO ZUCHAO DU LIZE HU FUDONG MEN SHIYING LI YINGJIE JI DONG HAN PENG CHEN GUOSHENG YUAN DONG HOU LEI |
description | The invention provides a robust attitude control method of a space interceptor. The method includes the following steps: step 1, establishing an aircraft attitude model; and step 2, designing a robustnonlinear attitude stabilization controller.
本发明提供了一种空间拦截器鲁棒姿态控制方法,包括以下步骤:步骤1,建立飞行器姿态模型步骤2,设计鲁棒非线性姿态稳定控制器。 |
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本发明提供了一种空间拦截器鲁棒姿态控制方法,包括以下步骤:步骤1,建立飞行器姿态模型步骤2,设计鲁棒非线性姿态稳定控制器。</description><language>chi ; eng</language><subject>CONTROLLING ; PHYSICS ; REGULATING ; SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><creationdate>2019</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191227&DB=EPODOC&CC=CN&NR=110618694A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20191227&DB=EPODOC&CC=CN&NR=110618694A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ZHOU CHENGBAO</creatorcontrib><creatorcontrib>LI RUXIANG</creatorcontrib><creatorcontrib>WANG GUOYOU</creatorcontrib><creatorcontrib>JIN KAIWEN</creatorcontrib><creatorcontrib>LU MINGKUI</creatorcontrib><creatorcontrib>WANG KUI</creatorcontrib><creatorcontrib>LI QICHANG</creatorcontrib><creatorcontrib>LIANG DONGDONG</creatorcontrib><creatorcontrib>BAO ZUCHAO</creatorcontrib><creatorcontrib>DU LIZE</creatorcontrib><creatorcontrib>HU FUDONG</creatorcontrib><creatorcontrib>MEN SHIYING</creatorcontrib><creatorcontrib>LI YINGJIE</creatorcontrib><creatorcontrib>JI DONG</creatorcontrib><creatorcontrib>HAN PENG</creatorcontrib><creatorcontrib>CHEN GUOSHENG</creatorcontrib><creatorcontrib>YUAN DONG</creatorcontrib><creatorcontrib>HOU LEI</creatorcontrib><title>Robust attitude control method of space interceptor</title><description>The invention provides a robust attitude control method of a space interceptor. The method includes the following steps: step 1, establishing an aircraft attitude model; and step 2, designing a robustnonlinear attitude stabilization controller.
本发明提供了一种空间拦截器鲁棒姿态控制方法,包括以下步骤:步骤1,建立飞行器姿态模型步骤2,设计鲁棒非线性姿态稳定控制器。</description><subject>CONTROLLING</subject><subject>PHYSICS</subject><subject>REGULATING</subject><subject>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAOyk8qLS5RSCwpySwpTUlVSM7PKynKz1HITS3JyE9RyE9TKC5ITE5VyMwrSS1KTi0oyS_iYWBNS8wpTuWF0twMim6uIc4euqkF-fGpYOV5qSXxzn6GhgZmhhZmliaOxsSoAQAqNyzX</recordid><startdate>20191227</startdate><enddate>20191227</enddate><creator>ZHOU CHENGBAO</creator><creator>LI RUXIANG</creator><creator>WANG GUOYOU</creator><creator>JIN KAIWEN</creator><creator>LU MINGKUI</creator><creator>WANG KUI</creator><creator>LI QICHANG</creator><creator>LIANG DONGDONG</creator><creator>BAO ZUCHAO</creator><creator>DU LIZE</creator><creator>HU FUDONG</creator><creator>MEN SHIYING</creator><creator>LI YINGJIE</creator><creator>JI DONG</creator><creator>HAN PENG</creator><creator>CHEN GUOSHENG</creator><creator>YUAN DONG</creator><creator>HOU LEI</creator><scope>EVB</scope></search><sort><creationdate>20191227</creationdate><title>Robust attitude control method of space interceptor</title><author>ZHOU CHENGBAO ; LI RUXIANG ; WANG GUOYOU ; JIN KAIWEN ; LU MINGKUI ; WANG KUI ; LI QICHANG ; LIANG DONGDONG ; BAO ZUCHAO ; DU LIZE ; HU FUDONG ; MEN SHIYING ; LI YINGJIE ; JI DONG ; HAN PENG ; CHEN GUOSHENG ; YUAN DONG ; HOU LEI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN110618694A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2019</creationdate><topic>CONTROLLING</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES</topic><toplevel>online_resources</toplevel><creatorcontrib>ZHOU CHENGBAO</creatorcontrib><creatorcontrib>LI RUXIANG</creatorcontrib><creatorcontrib>WANG GUOYOU</creatorcontrib><creatorcontrib>JIN KAIWEN</creatorcontrib><creatorcontrib>LU MINGKUI</creatorcontrib><creatorcontrib>WANG KUI</creatorcontrib><creatorcontrib>LI QICHANG</creatorcontrib><creatorcontrib>LIANG DONGDONG</creatorcontrib><creatorcontrib>BAO ZUCHAO</creatorcontrib><creatorcontrib>DU LIZE</creatorcontrib><creatorcontrib>HU FUDONG</creatorcontrib><creatorcontrib>MEN SHIYING</creatorcontrib><creatorcontrib>LI YINGJIE</creatorcontrib><creatorcontrib>JI DONG</creatorcontrib><creatorcontrib>HAN PENG</creatorcontrib><creatorcontrib>CHEN GUOSHENG</creatorcontrib><creatorcontrib>YUAN DONG</creatorcontrib><creatorcontrib>HOU LEI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ZHOU CHENGBAO</au><au>LI RUXIANG</au><au>WANG GUOYOU</au><au>JIN KAIWEN</au><au>LU MINGKUI</au><au>WANG KUI</au><au>LI QICHANG</au><au>LIANG DONGDONG</au><au>BAO ZUCHAO</au><au>DU LIZE</au><au>HU FUDONG</au><au>MEN SHIYING</au><au>LI YINGJIE</au><au>JI DONG</au><au>HAN PENG</au><au>CHEN GUOSHENG</au><au>YUAN DONG</au><au>HOU LEI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Robust attitude control method of space interceptor</title><date>2019-12-27</date><risdate>2019</risdate><abstract>The invention provides a robust attitude control method of a space interceptor. The method includes the following steps: step 1, establishing an aircraft attitude model; and step 2, designing a robustnonlinear attitude stabilization controller.
本发明提供了一种空间拦截器鲁棒姿态控制方法,包括以下步骤:步骤1,建立飞行器姿态模型步骤2,设计鲁棒非线性姿态稳定控制器。</abstract><oa>free_for_read</oa></addata></record> |
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subjects | CONTROLLING PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES |
title | Robust attitude control method of space interceptor |
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