论文标题

无人机通信的能源模型:实验验证和模型概括

Energy Model for UAV Communications: Experimental Validation and Model Generalization

论文作者

Gao, Ning, Zeng, Yong, Wang, Jian, Wu, Di, Zhang, Chaoyue, Song, Qingheng, Qian, Jiachen, Jin, Shi

论文摘要

涉及无人机(UAV)的无线通信预计将在未来的无线网络中发挥重要作用。但是,与传统的地面通信系统不同,无人机通常一方面具有有限的船上能源,另一方面需要额外的飞行能源消耗,这使能源效率高的无人机通信具有至高无上的智能能源消耗。在本文中,通过广泛的飞行实验,我们旨在首先验证旋转翼无人机的最近得出的理论能量模型,然后为那些复杂的飞行场景开发一个通用模型,在这些复杂的飞行场景中,严格的理论模型衍生是非常具有挑战性的,即使不是不可能的。具体来说,我们首先研究了无人机消耗如何随着其飞行速度而变化,以最简单的直飞航班。收集了大约12,000个有效的功率速度数据点,我们首先应用基于模型的曲线拟合,以根据现有文献中理论封闭形式的能量模型获得建模参数。此外,为了排除理论能量模型引起的潜在偏差,还使用无模型的深神经网络训练所获得的测量数据。发现从两种方法中获得的曲线都可以与理论能量模型很好地匹配。接下来,我们将研究进一步扩展到任意的二维(2-D)飞行,据我们所知,封闭形式的能量模型没有严格的理论推导,这是其飞行速度,方向和加速度的函数。为了填补空白,我们首先为这些更复杂的情况提出了一个启发式能量模型,然后根据循环水平飞行的测量结果提供实验验证。

Wireless communication involving unmanned aerial vehicles (UAVs) is expected to play an important role in future wireless networks. However, different from conventional terrestrial communication systems, UAVs typically have rather limited onboard energy on one hand, and require additional flying energy consumption on the other hand, which renders energy-efficient UAV communication with smart energy expenditure of paramount importance. In this paper, via extensive flight experiments, we aim to firstly validate the recently derived theoretical energy model for rotary-wing UAVs, and then develop a general model for those complicated flight scenarios where rigorous theoretical model derivation is quite challenging, if not impossible. Specifically, we first investigate how UAV power consumption varies with its flying speed for the simplest straight-and-level flight. With about 12,000 valid power-speed data points collected, we first apply the model-based curve fitting to obtain the modelling parameters based on the theoretical closed-form energy model in the existing literature. In addition, in order to exclude the potential bias caused by the theoretical energy model, the obtained measurement data is also trained using a model-free deep neural network. It is found that the obtained curve from both methods can match quite well with the theoretical energy model. Next, we further extend the study to arbitrary 2-dimensional (2-D) flight, where, to our best knowledge, no rigorous theoretical derivation is available for the closed-form energy model as a function of its flying speed, direction, and acceleration. To fill the gap, we first propose a heuristic energy model for these more complicated cases, and then provide experimental validation based on the measurement results for circular level flight.

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