Feasibility of varying geo-fence around an unmanned aircraft operation based on vehicle performance and wind

Sarah D'Souza, A. Ishihara, Ben E. Nikaido, Hashmatullah Hasseeb
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引用次数: 21

Abstract

Managing trajectory separation of unmanned aircraft is critical to ensuring accessibility, efficiency, and safety in low altitude airspace. The concept of a geo-fence has emerged as a way to manage trajectory separation. A geo-fence consists of distance buffers that enclose individual trajectories to identify a `keep-in' region and/or enclose areas that identify `keep-out' regions. The `keep-in' geo-fence size can be defined as a static number or calculated as a function of vehicle performance characteristics, state of the airspace, weather, and other unforeseen events such as emergency or disaster response. Given that the fleet of Unmanned Aircraft Systems (UAS) operating in low altitude airspace will be numerous and non-homogeneous, calculating a `keep-in' geo-fence will need to balance operational safety and efficiency. A recently tested UAS Traffic Management (UTM) prototype used a geo-fence size of 30 meters, horizontally and vertically, for every operation submitted. The goal of this work is to determine the feasibility of a generalized, simple algorithm that calculates geo-fence sizes as a function of vehicle performance and potential wind disturbances. The resulting geo-fence size could be smaller or larger because the vehicle performance in the presence of wind is considered, thus leading to trajectory separation that is safe and efficient. In this paper, two simplified methods were developed to determine the feasibility of calculating a geo-fence as a function of vehicle parameters and wind information. The first method calculates the geo-fence using basic vehicle parameters and wind sensor data in a set of algebraic-geometric equations. The second method models a generic PID control system that uses a simplified set of equations of motion for the plant and uses gain scheduling to account for wind disturbances. It was found that the Algebraic-Geometric Geo-fence Algorithm provides geo-fence sizes of approximately 15 meters horizontally and 5 meters vertically, which is much smaller than the UTM static value of 30 meters. In the PID Controller Geo-fence Algorithm it was found that the geo-fence size is further reduced to less than 5 meters, horizontally and vertically. These results reveal that implementing geo-fence calculations provide UTM with the ability to schedule and separate operations based on geofences that are dynamic to vehicle capability and environment, which is more efficient than using a single static geo-fence.
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基于车辆性能和风力变化的无人驾驶飞机周围地理围栏的可行性
管理好无人飞行器的轨迹分离是保证低空空域可达性、效率和安全的关键。地理围栏的概念是作为一种管理弹道分离的方法而出现的。地理围栏由距离缓冲区组成,它包围了单个轨迹,以识别“进入”区域和/或包围了识别“进入”区域的区域。“保持”地理围栏的大小可以定义为一个静态数字,也可以根据车辆性能特征、空域状态、天气和其他不可预见事件(如紧急情况或灾害响应)的函数来计算。考虑到在低空空域运行的无人机系统(UAS)数量众多且不均匀,计算“保持”地理围栏将需要平衡运行安全性和效率。最近测试的UAS交通管理(UTM)原型使用了30米大小的地理围栏,水平和垂直,用于提交的每个操作。这项工作的目标是确定一种通用的、简单的算法的可行性,该算法可以计算地理围栏尺寸作为车辆性能和潜在风干扰的函数。由于考虑了车辆在有风的情况下的性能,因此产生的地理围栏尺寸可以更小或更大,从而导致安全有效的轨迹分离。本文开发了两种简化的方法,以确定作为车辆参数和风信息的函数计算地理围栏的可行性。第一种方法是利用车辆基本参数和风传感器数据在一组代数几何方程中计算地护栏。第二种方法是建立一个通用的PID控制系统模型,该系统使用一组简化的植物运动方程,并使用增益调度来考虑风的干扰。研究发现,代数-几何Geo-fence算法提供的Geo-fence尺寸在水平方向上约为15米,在垂直方向上约为5米,远小于UTM静态值30米。在PID控制器Geo-fence算法中发现,无论在水平方向还是垂直方向,Geo-fence的尺寸都进一步减小到小于5米。这些结果表明,实施地理围栏计算为UTM提供了基于地理围栏的调度和分离操作的能力,这些地理围栏与车辆能力和环境是动态的,这比使用单个静态地理围栏更有效。
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