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Power and Weight Considerations in Small, Agile, Quadrotors

机译:小型,敏捷,四旋翼飞行器的功率和重量考虑

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The development of autonomous Micro Aerial Vehicles (MAVs) is significantly constrained by their size, weight and power consumption. In this paper, we explore the energetics of quadrotor platforms and study the scaling of mass, inertia, lift and drag with their characteristic length. The effects of length scale on masses and inertias associated with various components are also investigated. Additionally, a study of Lithium Polymer battery performance is presented in terms of specific power and specific energy. Finally, we describe the power and energy consumption for different quadrotors and explore the dependence on size and mass for static hover tests as well as representative maneuvers.
机译:自主微型飞行器(MAV)的发展受到其尺寸,重量和功耗的极大限制。在本文中,我们探索了四旋翼平台的能量学,并研究了其质量长度,惯性,升力和阻力的缩放比例。还研究了长度标度对与各种组件相关的质量和惯性的影响。此外,还根据比功率和比能量对锂聚合物电池的性能进行了研究。最后,我们描述了不同四旋翼飞机的功率和能量消耗,并探讨了静态悬停测试以及代表性机动对尺寸和质量的依赖性。

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