首页> 外文会议>2011 International Conference on Electronics, Communications and Control >Improved LQG control for small unmanned helicopter based on active model in uncertain environment
【24h】

Improved LQG control for small unmanned helicopter based on active model in uncertain environment

机译:不确定环境下基于活动模型的小型无人直升机改进LQG控制

获取原文
获取外文期刊封面目录资料

摘要

To make a small unmanned helicopter in an uncertain environment to stabilize the flight, in this paper, we take the active model and the LQG control combined, present a control method, it can effective adapt to model uncertainty. The method is hovering helicopter, from the helicopter dynamic model based on their own, the first design of LQR controller, followed modeling wind disturbed in uncertain environment, it is regarded as the disturbance of the force on the helicopter to helicopter dynamics model as a parameter, then through the Kalman filter joint estimation the states and parameters of the helicopter in order to achieve the reconstruction of the controller. The simulation results based on single channel confirmed the effectiveness of this control method.
机译:为了使小型无人直升机在不确定的环境中稳定飞行,本文采用主动模型和LQG控制相结合,提出一种控制方法,可以有效地适应模型的不确定性。悬停直升机的方法是,从自身的直升机动态模型出发,首先设计LQR控制器,然后对不确定环境中的风扰动进行建模,将直升机上的力扰动视为直升机动力学模型的一个参数。 ,然后通过卡尔曼滤波器联合估计直升机的状态和参数,以实现对控制器的重构。基于单通道的仿真结果证实了该控制方法的有效性。

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