论文标题

辅助便携式接入点的节能轨迹设计

Energy-Efficient Trajectory Design of a Multi-IRS Assisted Portable Access Point

论文作者

Babu, Nithin, Virgili, Marco, Al-jarrah, Mohammad, Jing, Xiaoye, Alsusa, Emad, Popovski, Petar, Forsyth, Andrew, Masouros, Christos, Papadias, Constantinos B.

论文摘要

在这项工作中,我们提出了一个无人驾驶飞机(UAV)的便携式访问点(PAP)的框架,用于服务一组地面节点(GNS)。除PAP和GNS外,该系统还由安装在人造结构上的一组智能反射表面(IRS)组成,以增加每次消耗的能源消耗的钻头数量,这些能量消耗被测量为全球能量效率(GEE)。 PAP的GEE轨迹是通过考虑无人机推进能量消耗和PAP电池的PEUKERT效应来设计的,PAP电池代表了精确的电池放电曲线作为无人机功耗概况的非线性功能。 GEE轨迹设计问题分为两个阶段:在第一个阶段中,使用多层圆圈填料方法发现了PAP的路径和IRS模块的可行位置,并使用替代优化方法计算出所需的IRS相移值,该方法是考虑了IRS元素的振幅和相位响应之间的相互依赖性;在第二阶段,使用新型的多轨迹设计算法计算PAP飞行速度和用户调度。数值评估表明:忽略Peukert效应高估了PAP的可用飞行时间;一定的阈值后,增加电池尺寸会减少PAP的可用飞行时间;与其他基线场景相比,IRS模块的存在改善了系统的GEE。与使用顺序凸编程和Dinkelbach算法的组合开发的单圈轨迹相比,多圈轨迹可节省更多的能量。

In this work, we propose a framework for energy-efficient trajectory design of an unmanned aerial vehicle (UAV)-based portable access point (PAP) deployed to serve a set of ground nodes (GNs). In addition to the PAP and GNs, the system consists of a set of intelligent reflecting surfaces (IRSs) mounted on man-made structures to increase the number of bits transmitted per Joule of energy consumed measured as the global energy efficiency (GEE). The GEE trajectory for the PAP is designed by considering the UAV propulsion energy consumption and the Peukert effect of the PAP battery, which represents an accurate battery discharge profile as a non-linear function of the UAV power consumption profile. The GEE trajectory design problem is solved in two phases: in the first, a path for the PAP and feasible positions for the IRS modules are found using a multi-tier circle packing method, and the required IRS phase shift values are calculated using an alternate optimization method that considers the interdependence between the amplitude and phase responses of an IRS element; in the second phase, the PAP flying velocity and user scheduling are calculated using a novel multilap trajectory design algorithm. Numerical evaluations show that: neglecting the Peukert effect overestimates the available flight time of the PAP; after a certain threshold, increasing the battery size reduces the available flight time of the PAP; the presence of IRS modules improves the GEE of the system compared to other baseline scenarios; the multi-lap trajectory saves more energy compared to a single-lap trajectory developed using a combination of sequential convex programming and Dinkelbach algorithm.

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