Event trigger based nonlinear flight control for a small size unmanned helicopter

被引:0
|
作者
Gu, Xun [1 ,2 ]
Xian, Bin [1 ]
Zhang, Xu [1 ]
机构
[1] Tianjin Univ, Inst Robot & Autonomous Syst, Sch Elect & Informat Engn, Tianjin 30072, Peoples R China
[2] Guiyang Univ, Sch Elect & Commun Engn, Guiyang 55000, Guizhou, Peoples R China
基金
国家重点研发计划; 中国国家自然科学基金;
关键词
event trigger; nonlinear controller; unmanned helicopter; numerical simulation; TRACKING CONTROL;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Compared with the traditional periodic control methodology, the event trigger based control strategy is an advanced control strategy to make optimal utilization of resources while remaining the control performance at the same time. In this paper, the limited on board computing resource is considered, and the event trigger based nonlinear control strategy is proposed for a small size unmanned helicopter under the effect of the unknown external disturbances. The stability of the control strategy is proved via the Lyapunov based analysis, and the effectiveness of the proposed control strategy is verified via the numerical simulation The simulation results show that the proposed event trigger based control strategy has a good attitude tracking performance under the effect of the unknown external disturbances while reducing the computing resources greatly.
引用
收藏
页码:334 / 339
页数:6
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