期刊
EUROPEAN JOURNAL OF CONTROL
卷 48, 期 -, 页码 97-103出版社
ELSEVIER SCIENCE BV
DOI: 10.1016/j.ejcon.2018.11.003
关键词
Spacecraft formation attitude consensus; Actuator faults; Sliding mode control; Event-triggered control
资金
- National Natural Science Foundation of China [91438202, 61833009, 61473096, 61690212, 61333003]
- Open Fund of National Defense Key Discipline Laboratory of Micro-Spacecraft Technology [HIT.KLOF.MST.201701]
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.
作者
我是这篇论文的作者
点击您的名字以认领此论文并将其添加到您的个人资料中。
推荐
暂无数据