首页> 外文会议>Chinese Intelligent Systems Conference >Chapter 25 Fault Tolerant Tracking Control for a Team of Non-Minimum Phase VTOL Aircrafts Based on Virtual Leader Structure
【24h】

Chapter 25 Fault Tolerant Tracking Control for a Team of Non-Minimum Phase VTOL Aircrafts Based on Virtual Leader Structure

机译:基于虚拟领导结构的非最小相位VTOL飞机团队的故障跟踪控制

获取原文

摘要

This paper develops a fault tolerant approach for a team of thrust vector vertical take-off and landing (VTOL) aircrafts based on virtual leader structure. First, for each VTOL aircraft, a cascaded observer system with two extended state fault diagnosis observers (ESFDO) is designed. Then, local fault tolerant tracking controllers are developed. Finally, simulation results for a team of three VTOL aircrafts are presented to demonstrate the effectiveness of our proposed method.
机译:本文对基于虚拟领导结构的推力矢量垂直起飞和着陆(VTOL)飞机的团队开发了一种容错方法。首先,对于每个VTOL飞机,设计了具有两个扩展状态故障诊断观察员(ESFDO)的级联观察者系统。然后,开发了本地容错跟踪控制器。最后,提出了三个VTOL飞机团队的仿真结果,以证明我们提出的方法的有效性。

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