空间控制技术与应用2018，Vol.44Issue(2)：31-35,41,6.DOI:10.3969/j.issn.1674-1579.2018.02.006
基于事件触发的航天器变周期控制方法研究
Aperiodic Spacecraft Control Method:An Event Triggered Approach
摘要
Abstract
Future spacecraft will have much autonomous work.And the utilization of embedded system continues growing with data increasing.In this paper,a nonlinear event triggered control approach is ap-plied for the spacecraft attitude control.By this approach, the utilization of bus bandwidth decreases greatly and a good control performance is achieved.Moreover,the design procedure and stability proof of this algorithm are given via perturbation theorem.Finally, a numerical example is provided to illustrate the efficiency and feasibility of the proposed approach.关键词
信息物理系统/事件触发控制/姿态控制/总线带宽Key words
cyber-physical system/event-triggered control/attitude control/bus bandwidth分类
航空航天引用本文复制引用
孙帅,王磊,王志文..基于事件触发的航天器变周期控制方法研究[J].空间控制技术与应用,2018,44(2):31-35,41,6.基金项目
国家高技术研究发展计划(863)资助项目(2015AA7046306).Supported by National High-Tech R&D(863)Program(2015AA7046306). （863）
