Quadrotors with Slung Payloads: Energy Analysis and Experimental Validation

Hassan Alkomy, J. Shan
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Abstract

This paper analyzes the energy consumption of quadrotors with slung payloads. First, it develops novel expressions for the power and energy consumption for a quadrotor with a slung payload flying in 3D. These expressions are called the power and energy quotients, which are directly proportional to the actual power and energy consumption. However, they do not require any prior knowledge of the motor and propeller parameters. Second, a comprehensive energy investigation is conducted to find the effect of polynomial trajectories, cable length, arbitrary kinematic boundary conditions, and number of waypoints on the energy consumption. This analysis has been conducted via two different Monte Carlo simulations. The results showed that increasing the degree of the polynomial trajectory increases the energy consumption and there is an optimal cable length, at which, the energy consumption is minimal. These results are valid regardless of the kinematic boundary conditions, which implies that these results are valid regardless of the number of waypoints. All results have been validated experimentally.
悬挂式四旋翼飞行器:能量分析与实验验证
本文分析了悬挂式四旋翼飞行器的能量消耗。首先,它开发了新的表达式的功率和能量消耗的四旋翼与悬挂载荷飞行在三维。这些表达式被称为功率和能量商,它与实际功率和能量消耗成正比。然而,他们不需要电机和螺旋桨参数的任何先验知识。其次,进行了全面的能量调查,找出多项式轨迹、电缆长度、任意运动边界条件和路径点数量对能量消耗的影响。该分析是通过两种不同的蒙特卡罗模拟进行的。结果表明,随着多项式轨迹度的增加,电缆能耗也随之增加,且存在一个最优电缆长度,此时电缆能耗最小。这些结果是有效的,无论运动学边界条件,这意味着这些结果是有效的,无论路径点的数量。所有结果均经过实验验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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