首页> 外文期刊>European Journal of Control >Event-triggered fault tolerant control for spacecraft formation attitude synchronization with limited data communication
【24h】

Event-triggered fault tolerant control for spacecraft formation attitude synchronization with limited data communication

机译:事件触发的容错控制,用于有限数据通信的航天器编队姿态同步

获取原文
获取原文并翻译 | 示例
           

摘要

This paper investigates the leader-following attitude consensus problem of a group of n-th spacecrafts with actuator fault and limited data communication, where the event-triggered based sending mechanism is considered to decrease communication burthen. In this design, unknown actuator faults and external disturbances are considered, and an event-triggered based adaptive distributed cooperative attitude control law is developed to solve the multiple spacecrafts formation control problem. It is shown that leader-following attitude synchronization can be achieved under the designed event-triggered control law. Finally, a simulation example is provided to illustrate the effectiveness of the proposed attitude coordination control techniques. (C) 2018 European Control Association. Published by Elsevier Ltd. All rights reserved.
机译:本文研究了一组第n个执行器故障且数据通信受限的航天器的前导跟随姿态共识问题,其中考虑了基于事件触发的发送机制,以减少通信负担。在该设计中,考虑了未知的致动器故障和外部干扰,并开发了一种基于事件触发的自适应分布式协作姿态控制律,以解决多种航天器编队控制问题。结果表明,在设计的事件触发控制律下,可以实现领导者跟随态度的同步。最后,提供了一个仿真示例来说明所提出的姿态协调控制技术的有效性。 (C)2018欧洲控制协会。由Elsevier Ltd.出版。保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号