Global fast dynamic terminal sliding mode control for a quadrotor UAV
详细信息    查看全文
文摘
A control method is proposed for a quadrotor UAV. The global fast dynamic terminal sliding mode control technique is used. The technique can ensure the state tracking errors converge to zero in finite time. The proposed control method can eliminate the chattering phenomenon on controller.

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700