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Distributed attitude synchronization control for multiple flexible spacecraft without modal variable measurement

机译:多个柔性航天器的分布式姿态同步控制,无模块变量测量

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摘要

Summary >This paper solves the attitude synchronization and tracking problem for a group of flexible spacecraft without flexible‐mode variable measurement. The spacecraft formation is studied in a leader‐following synchronization scheme with a dynamic virtual leader. With the application of adaptive sliding‐mode control technique, a distributed modified Rodriguez parameters‐based dynamic controller is proposed for flexible spacecraft without requiring modal variable measurement. It is proved that the attitude synchronization and tracking can be achieved asymptotically under the control strategy through the Lyapunov's stability analysis. Furthermore, a distributed robust continuous control algorithm is designed to guarantee the ultimate boundedness of both the attitude tracking error and the modal variable observation error when bounded external disturbances exist. Some numerical simulation examples for multiple flexible spacecraft formation are given to demonstrate the effectiveness of the proposed method. </abstract> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> <div class="translation abstracttxt"> <span class="zhankaihshouqi fivelineshidden" id="abstract"> <span>机译:</span><abstract xmlns =“http://www.wiley.com/namespaces/wiley”type =“main”xml:lang =“en”xml:id =“rnc4092-abs-abs-0001”> <标题类型=“main” >摘要</ title> >本文解决了一组柔性航天器而无需灵活模式变量测量的姿态同步和跟踪问题。在带有动态虚拟领导者的领导者之后的同步方案中研究了航天器形成。随着自适应滑模控制技术的应用,为柔性航天器提出了一种基于分布式修改的Rodriguez参数的动态控制器,而无需模态变量测量。事实证明,通过Lyapunov的稳定性分析,可以在控制策略下实现态度同步和跟踪。此外,分布式稳健的连续控制算法旨在保证当存在有界外部干扰时姿态跟踪误差和模态变量观察误差的最终界限。用于多种柔性航天器形成的一些数值模拟实施例,证明了所提出的方法的有效性。</ p> </摘要> </span> <span class="z_kbtn z_kbtnclass hoverxs" style="display: none;">展开▼</span> </div> </div> <div class="record"> <h2 class="all_title" id="enpatent33" >著录项</h2> <ul> <li> <span class="lefttit">来源</span> <div style="width: 86%;vertical-align: text-top;display: inline-block;"> <a href='/journal-foreign-21736/'>《International Journal of Robust and Nonlinear Control》</a> <b style="margin: 0 2px;">|</b><span>2018年第10期</span><b style="margin: 0 2px;">|</b><span>共19页</span> </div> </li> <li> <div class="author"> <span class="lefttit">作者</span> <p id="fAuthorthree" class="threelineshidden zhankaihshouqi"> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Wang Qishao&option=202" target="_blank" rel="nofollow">Wang Qishao;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Duan Zhisheng&option=202" target="_blank" rel="nofollow">Duan Zhisheng;</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Lv Yuezu&option=202" target="_blank" rel="nofollow">Lv Yuezu;</a> </p> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zkzz" style="display: none;">展开▼</span> </div> </li> <li> <div style="display: flex;"> <span class="lefttit">作者单位</span> <div style="position: relative;margin-left: 3px;max-width: 639px;"> <div class="threelineshidden zhankaihshouqi" id="fOrgthree"> <p>State Key Laboratory for Turbulence and Complex Systems Department of Mechanics and Engineering ScienceCollege of Engineering Peking UniversityBeijing China;</p> <p>State Key Laboratory for Turbulence and Complex Systems Department of Mechanics and Engineering ScienceCollege of Engineering Peking UniversityBeijing China;</p> <p>State Key Laboratory for Turbulence and Complex Systems Department of Mechanics and Engineering ScienceCollege of Engineering Peking UniversityBeijing China;</p> </div> <span class="z_kbtnclass z_kbtnclassall hoverxs" id="zhdw" style="display: none;">展开▼</span> </div> </div> </li> <li > <span class="lefttit">收录信息</span> <span style="width: 86%;vertical-align: text-top;display: inline-block;"></span> </li> <li> <span class="lefttit">原文格式</span> <span>PDF</span> </li> <li> <span class="lefttit">正文语种</span> <span>eng</span> </li> <li> <span class="lefttit">中图分类</span> <span><a href="https://www.zhangqiaokeyan.com/clc/7742.html" title="自动化系统">自动化系统;</a></span> </li> <li class="antistop"> <span class="lefttit">关键词</span> <p style="width: 86%;vertical-align: text-top;"> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=adaptive control&option=203" rel="nofollow">adaptive control;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=attitude synchronization&option=203" rel="nofollow">attitude synchronization;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=flexible spacecraft&option=203" rel="nofollow">flexible spacecraft;</a> <a style="color: #3E7FEB;" href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=sliding mode&option=203" rel="nofollow">sliding mode;</a> </p> <div class="translation"> 机译:自适应控制;姿态同步;灵活的航天器;滑模; </div> </li> </ul> </div> </div> <div class="literature cardcommon"> <div 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<span>1989</span> </span> </div> <p class="zwjiyix translation" style="max-width: initial;height: auto;word-break: break-all;white-space: initial;text-overflow: initial;overflow: initial;"> <span>机译:柔性航天器的变结构姿态控制与弹性模态稳定。</span> </p> </li> </ul> <ul style="display: none;"> <li> <div> <b>1. </b><a class="enjiyixqcontent" href="/academic-journal-cn_journal-dynamics-control_thesis/0201229065174.html">充液柔性航天器非线性姿态动力学及再定向姿态机动</a> <b>[J]</b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=岳宝增&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 岳宝增</a> <span> <a href="/journal-cn-10432/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 动力学与控制学报 </a> </span> <span> . 2010</span><span>,第001期</span> </span> </div> </li> <li> <div> <b>2. </b><a class="enjiyixqcontent" href="/academic-journal-cn_journal-xuzhou-institute-technology-natural-sciences-edition_thesis/020127889824.html">基于Adomian分解法的分数阶航天器姿态动力系统的求解与同步控制</a> <b>[J]</b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=陈恒&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 陈恒</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=雷腾飞&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,雷腾飞</a> <span> <a href="/journal-cn-7420/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 徐州工程学院学报(自然科学版) </a> </span> <span> . 2017</span><span>,第003期</span> </span> </div> </li> <li> <div> <b>3. </b><a class="enjiyixqcontent" href="/academic-journal-cn_journal-harbin-institute-technology_thesis/0201234505473.html">在轨服务航天器对失控目标的姿态同步控制</a> <b>[J]</b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=耿云海&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 耿云海</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=卢伟&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,卢伟</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=陈雪芹&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,陈雪芹</a> <span> <a href="/journal-cn-11626/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 哈尔滨工业大学学报 </a> </span> <span> . 2012</span><span>,第001期</span> </span> </div> </li> <li> <div> <b>4. </b><a class="enjiyixqcontent" href="/academic-journal-cn_control-engineering-beijing_thesis/0201224897899.html">利用GPS姿态敏感器和星敏感器测量值的组合确定航天器的姿态</a> <b>[J]</b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Christian&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . Christian</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Arbinger&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,Arbinger</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=Werner&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,Werner</a> <span> <a href="/journal-cn-23921/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 控制工程(北京) </a> </span> <span> . 2005</span><span>,第004期</span> </span> </div> </li> <li> <div> <b>5. </b><a class="enjiyixqcontent" href="/academic-journal-cn_chinese-space-science-technology_thesis/0201271234015.html">基于同波束干涉测量的航天器姿态测量研究</a> <b>[J]</b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=张天刚&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 张天刚</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=任天鹏&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,任天鹏</a> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=谢剑锋&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor">,谢剑锋</a> <span> <a href="/journal-cn-9943/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 中国空间科学技术 </a> </span> <span> . 2019</span><span>,第002期</span> </span> </div> </li> <li> <div> <b>6. </b><a class="enjiyixqcontent" href="/academic-conference-cn_meeting-16944_thesis/020221735134.html">柔性充液航天器姿态转换机动及混沌姿态控制</a> <b>[C]</b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=岳宝增&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 岳宝增</a> <span> <a href="/conference-cn-16944/" target="_blank" rel="nofollow" class="tuijian_authcolor"> . 第十二届全国非线性振动暨第九届全国非线性动力学和运动稳定性学术会议 </a> <span> <span> . 2009</span> </span> </div> </li> <li> <div> <b>7. </b><a class="enjiyixqcontent" href="/academic-degree-domestic_mphd_thesis/020316274171.html">太阳帆航天器悬浮轨道保持与柔性姿态控制研究</a> <b>[A] </b> <span> <a href="/search.html?doctypes=4_5_6_1-0_4-0_1_2_3_7_9&sertext=陈弈澄&option=202" target="_blank" rel="nofollow" class="tuijian_auth tuijian_authcolor"> . 陈弈澄</a> <span> . 2020</span> </span> </div> </li> </ul> <ul style="display: none;"> <li> <div> <b>1. </b><a class="enjiyixqcontent" href="/patent-detail/061204484575.html">一种姿态控制与姿态测量分时复用的航天器姿态控制方法</a> <b>[P]</b> . <span> 中国专利: CN108897336B </span> <span> . 2021.06.22</span> </div> </li> <li> <div> <b>2. </b><a class="enjiyixqcontent" href="/patent-detail/06120111376130.html">一种姿态控制与姿态测量分时复用的航天器姿态控制方法</a> <b>[P]</b> . <span> 中国专利: CN108897336A </span> <span> . 2018-11-27</span> </div> </li> <li> <div> <b>3. </b><a class="enjiyixqcontent" href="/patent-detail/06130449758317.html">Methods for controlling spacecraft attitudes without exciting spacecraft resonances</a> <b>[P]</b> . <span> 外国专利: <!-- 美国专利: --> US6076772A </span> <span> 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