论文标题

为多旋转无人机建模功耗

Modelling Power Consumptions for Multi-rotor UAVs

论文作者

Gong, Hao, Huang, Baoqi, Jia, Bing, Dai, Hansu

论文摘要

无人驾驶汽车(UAV)具有各种优势,但其实际应用受其能源有限的影响。因此,管理其功耗很重要,并且建立相应的功耗模型也很重要。但是,大多数现有作品要么为固定翼无人机和单旋风无人机建立理论功耗模型,要么为无需严格的数学推导而为多旋转无人机提供启发式功耗模型。本文旨在为多旋转无人机建立理论功耗模型。具体来说,在三个飞行状态,即前飞行,垂直上升和垂直下降的封闭形式的功耗模型是通过利用单人无人机与多旋翼无人机在功率消费方面的关系来得出的。在此基础上,在三维(3-D)方案中,无人机的通用飞行功耗模型。通过使用DJI M210和DJI移动SDK在实际场景中制作的移动应用程序进行广泛的实验,并确认这些模型的正确性和有效性;此外,进行仿真以进一步研究转子数量对无人机的功耗的影响。拟议的功耗模型不仅揭示了多旋转无人机的功耗如何受到各种因素的影响,而且还为引入其他新型应用程序铺平了道路。

Unmanned aerial vehicles (UAVs) have various advantages, but their practical applications are influenced by their limited energy. Therefore, it is important to manage their power consumption and also important to establish corresponding power consumption models. However, most of existing works either establish theoretical power consumption models for fixed-wing UAVs and single-rotor UAVs, or provide heuristic power consumption models for multi-rotor UAVs without rigorous mathematical derivations. This paper aims to establish theoretical power consumption models for multi-rotor UAVs. To be specific, the closed-form power consumption models for a multi-rotor UAV in three flight statuses, i.e., forward flight, vertical ascent and vertical descent, are derived by leveraging the relationship between single-rotor UAVs and multi-rotor UAVs in terms of power consumptions. On this basis, a generic flight power consumption model for the UAV in a three-dimensional (3-D) scenario is obtained. Extensive experiments are conducted by using DJI M210 and a mobile app made by DJI Mobile SDK in real scenarios, and confirm the correctness and effectiveness of these models; in addition, simulations are performed to further investigate the effect of the rotor numbers on the power consumption for the UAV. The proposed power consumption models not only reveal how the power consumption of multi-rotor UAVs are affected by various factors, but also pave the way for introducing other novel applications.

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