...
首页> 外文期刊>Journal of Intelligent & Robotic Systems: Theory & Application >Advances in Modeling and Control of Tethered Unmanned Helicopters to Enhance Hovering Performance
【24h】

Advances in Modeling and Control of Tethered Unmanned Helicopters to Enhance Hovering Performance

机译:系留无人直升机的建模和控制以增强悬停性能的研究进展

获取原文
获取原文并翻译 | 示例
           

摘要

The hovering capabilities of unmanned helicopters can be seriously affected by wind. One possible solution for improving hovering performance under such circumstances is the use of a tethered setup that takes advantage of the tension exerted on the cable that links the helicopter to the ground. This paper presents a more elaborate strategy for helicopter control in this augmented setup, that extends previous work on the subject by the authors. Particularly, a combination of classical PID control laws, together with model inversion blocks, constitutes the basis of the new controller. Additionally, feed-forward action for counteracting rotational couplings is also taken into account. The resulting nonlinear control structure considers also a viscoelastic model of the tether which accurately reproduce the behavior of real ropes. Several simulations under artificially generated wind influences are presented to endorse the validity of the new proposed controller.
机译:无人直升机的悬停能力会受到风的严重影响。在这种情况下提高悬停性能的一种可能的解决方案是使用系留装置,该装置利用施加在将直升机连接到地面的电缆上的张力。本文介绍了在这种扩展设置中用于直升机控制的更为精细的策略,该策略扩展了作者先前在该主题上的工作。特别是,经典PID控制定律与模型求逆模块的组合构成了新控制器的基础。另外,还考虑了用于抵消旋转联接的前馈作用。最终的非线性控制结构还考虑了系绳的粘弹性模型,该模型可以精确地再现真实绳索的行为。在人为产生的风影响下进行了几种仿真,以验证新提出的控制器的有效性。

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