首页> 外文期刊>IEEE Transactions on Robotics >Universal Flying Objects: Modular Multirotor System for Flight of Rigid Objects
【24h】

Universal Flying Objects: Modular Multirotor System for Flight of Rigid Objects

机译:通用飞行物体:用于刚性物体飞行的模块化多电流系统

获取原文
获取原文并翻译 | 示例
           

摘要

In this article, we introduce Universal Flying Objects—a modular aerial robotic platform for transforming a rigid object into a multirotor robot. To achieve this, we develop flight modules, in the form of a control module and propelling modules that can be affixed to an object. The object, or payload, serves as the airframe of the vehicle. The modular design produces a highly versatile platform as it is reconfigurable by the addition or removal of flight modules, adjustment of the modules’ arrangement, or change of payloads. To facilitate the flight control, we propose an inertial measurement unit (IMU)-based estimation strategy for rapid computation of the robot's configuration. When combined with the adaptive geometric controller for further refinement of uncertain parameters, stable flights are accomplished with minimal manual intervention or tuning required by a user. To this end, we demonstrate hovering and trajectory tracking flights through various robot configurations with different dummy payloads, weighing $pprox$200–800 g, using four to eight propelling modules. The results reveal that stable flights are attainable thanks to the proposed IMU-based estimation method. The flight performance is markedly improved over time through the adaptive scheme, with position errors of a few centimeters after the parameter convergence.
机译:在本文中,我们介绍了通用飞行物体 - 一个模块化空中机器人平台,用于将刚性物体转换为多电机机器人。为实现这一目标,我们以控制模块的形式和可以贴入对象的推进模块开发飞行模块。物体或有效载荷用作车辆的机身。模块化设计产生高度通用的平台,因为它可以通过添加或移除飞行模块来重新配置,调整模块的布置或有效载荷的变化。为了便于飞行控制,我们提出了一种惯性测量单元(IMU),用于快速计算机器人配置的估计策略。当与自适应几何控制器组合以进一步改进不确定参数时,通过用户需要最小的手动干预或调整,完成稳定的飞行。为此,我们展示了通过各种机器人配置的悬停和轨迹跟踪航班,具有不同的虚拟有效载荷,称重<内联公式XMLNS:MML =“http://www.w3.org/1998/math/mathml”xmlns:xlink =“http://www.w3.org/1999/xlink”> $ 左右$ 200-800 g,使用四到八个推进模块。结果表明,由于所提出的基于IMU的估计方法,可以实现稳定的航班。通过自适应方案随着时间的推移显着提高了飞行性能,在参数收敛后的位置误差为几厘米。

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