带有旋转跷跷板的全驱动无人机

Dolev Yecheskel, S. Arogeti
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引用次数: 0

摘要

标准无人机通常是欠驱动系统,这一特性限制了它们的机动能力。这种限制是由于总推力方向和无人机体的角状态之间的固有耦合。为了解耦这些量,我们建议使用跷跷板,这样可以独立控制推力方向。与其他基于额外执行机构来倾斜推力的结构不同,我们的解决方案不需要任何额外的执行机构来增加升力。提出的配置是一个八轴直升机与八个螺旋桨和四个跷跷板。这些结果扩展了先前基于单个跷跷板的建议结构。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A Fully-Actuated Drone with Rotating Seesaws
Standard drones are generally underactuated systems, an attribute that limits their maneuvering ability. This limitation is because of the inherent coupling between the total thrust direction and the angular state of the drone body. To decouple these quantities, we suggest using seesaws, which allow controlling the thrust direction independently. Unlike other structures based on additional actuators to tilt the thrust, our solution is not based on any extra actuator that does not contribute to the lifting force. The presented configuration is an octocopter with eight propellers and four seesaws. These results extend a former suggested structure based on a single seesaw.
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