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通信受限下基于终端滑模和指对数滑模方法的编队航天器姿态协同控制
投稿时间:2020-10-15    点此下载全文
引用本文:易航,陈雪芹,刘明.通信受限下基于终端滑模和指对数滑模方法的编队航天器姿态协同控制[J].南京信息工程大学学报,2021,13(1):29~40
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作者单位E-mail
易航 哈尔滨工业大学 航天学院, 哈尔滨, 150001  
陈雪芹 哈尔滨工业大学 航天学院, 哈尔滨, 150001 cxqhit@163.com 
刘明 哈尔滨工业大学 航天学院, 哈尔滨, 150001  
基金项目:国家自然科学基金(61833009,11972130,61690212)
中文摘要:针对星间通信时延和信号量化情形下编队航天器,研究对应的姿态协同控制器设计问题.首先,为节省编队航天器星间通信的带宽资源,提出基于信号量化的星间数据通信策略,并设计了一种终端滑模姿态协同控制器以保证航天器编队姿态同步系统的渐近稳定;其次,考虑到航天器间可能存在通信时延,考虑基于信号量化的通信策略,提出一种基于指对数滑模面的编队航天器协同控制器设计方法,能保证编队航天器在有限时间内达到期望姿态;最后基于包含4个航天器的编队系统,通过仿真验证了所提出的协同控制方法的有效性.
中文关键词:航天器编队  姿态协同控制  终端滑模控制  指数对数滑模控制  网络化控制
 
Cooperative attitude control for spacecraft formation with limited communication based on terminal and exponent-logarithmic sliding mode
Abstract:The cooperative attitude control is addressed for spacecraft formation with unreliable communication and signal quantization among spacecrafts.First,to save the data rate and bandwidth among the spacecrafts,a signal quantization communication strategy is proposed among each two spacecrafts in the formation,and a terminal sliding mode attitude control law is developed to ensure the asymptotic stability of the spacecraft formation attitude synchronization systems.Second,to compensate the effects of communication delay and signal quantization,an exponent-logarithmic sliding mode surface design is presented,based on which a cooperative attitude control strategy is developed for spacecraft formation to achieve desirable attitude in finite-time.Finally,a simulation example with four spacecrafts in a formation system is provided to verify the effectiveness of the proposed cooperative control method.
keywords:spacecraft formation  cooperative attitude control  terminal sliding mode control  exponent-logarithmic sliding mode control  networked control
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