首页> 外文会议>International Conference on Unmanned Aircraft Systems >Attitude and altitude control on board of an ornithopter
【24h】

Attitude and altitude control on board of an ornithopter

机译:奥尼托特船上的态度和高度控制

获取原文

摘要

This paper presents the modeling, the design of control laws, for Euler angles and altitude, and their implementation. The proposed controller is based on the backstepping procedure and uses a state feedback linearizing technique to guarantee tracking of the desired Euler angles and altitude on the ornithopter. The provided controller provides exponential convergence to the desired values. Numerical and experimental applications of the proposed algorithm illustrates the performance of the control technique.
机译:本文介绍了欧拉角度和高度的造型,控制法的设计及其实施。所提出的控制器基于BackStepping程序,并使用状态反馈线性化技术来保证在Ornithopter上跟踪所需的欧拉角和高度。提供的控制器为所需值提供指数趋势。所提出的算法的数值和实验应用说明了控制技术的性能。

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