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arXiv 1601.00733physics.flu-dynphysics.class-ph
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四旋翼桨叶的空气动力学

Aerodynamics of Rotor Blades for Quadrotors

Moses Bangura, Marco Melega, Roberto Naldi, Robert Mahony

摘要:

在这份报告中,我们提出了理论上的四旋翼空气动力学使用完善的动量和叶片元素的理论。从机器人的角度来看,推力和水平力和扭矩(因此功率)模型的理论发展是在四旋翼的机身固定框架中进行的。利用动量理论,我们提出并模拟了水平力及其相关功率的存在。考虑到动量理论的局限性和该理论不足以解释所提出的键合图中所表示的不同功率,导致使用叶片元件理论。使用这个理论,模型,然后开发不同的四旋翼转子的几何形状和空气动力学特性,包括最佳的悬停转子上使用的大多数四旋翼。虽然这种转子被证明是最佳的转子,我们表明,几何变化是必要的叶片的制造。几何形状的变化还取决于所需的推力与水平力之比,该推力与水平力之比基于可用的马达扭矩(因此功率)和飞行器的所需飞行包线。然后,将针对不同几何构型和翼型截面的空气动力学特性使用叶素理论获得的详细空气动力学模型转换为可用于机器人应用的集总参数模型。这些应用包括但不限于机身固定坐标系速度估算和单个转子推力调节[1,2]。

英文摘要:

In this report, we present the theory on aerodynamics of quadrotors using the well established momentum and blade element theories. From a robotics perspective, the theoretical development of the models for thrust and horizontal forces and torque (therefore power) are carried out in the body fixed frame of the quadrotor. Using momentum theory, we propose and model the existence of a horizontal force along with its associated power. Given the limitations associated with momentum theory and the inadequacy of the theory to account for the different powers represented in a proposed bond graph lead to the use of blade element theory. Using this theory, models are then developed for the different quadrotor rotor geometries and aerodynamic properties including the optimum hovering rotor used on the majority of quadrotors. Though this rotor is proven to be the most optimum rotor, we show that geometric variations are necessary for manufacturing of the blades. The geometric variations are also dictated by a desired thrust to horizontal force ratio which is based on the available motor torque (hence power) and desired flight envelope of the vehicle. The detailed aerodynamic models obtained using blade element theory for different geometric configurations and aerodynamic properties of the aerofoil sections are then converted to lumped parameter models that can be used for robotic applications. These applications include but not limited to body fixed frame velocity estimation and individual rotor thrust regulation [1, 2].

机构、总结、中文摘要均由AI分析而来,可能存在错误,请以论文正文为准。

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