Optimization of three-dimensional waypoint ordering for energy-optimal multirotor operation

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Nicolas Michel , Ayush Patnaik , Peng Wei , Zhaodan Kong , Xinfan Lin
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Abstract

Air mobility enabled by multirotor aircraft is an emerging transportation mode with wide real-world applications. Maximum range and flight duration are critical aspects of the performance, governed by the vehicle energy efficiency. This paper studies the energy-optimal planning of the multirotor, which aims at finding the optimal ordering of waypoints with the minimum energy consumption for missions in 3D space. The study uses a system model capturing first-principle energy dynamics of the multirotor. It is found that in most cases (up to 95%) the energy-optimal order is different from the minimum-distance order, which is the solution to the traditional traveling salesman problem. The difference can be as high as 14.9%, with the average at 1.6%-3.4% and 90th percentile at 3.8%-6.6% depending on the range and other parameters of the mission. To validate these results, three sample missions were tested in real-world flight, and the minimum-energy order was shown to reduce energy cost by 3.9%-9.4% relative to the minimum-distance order. These results were used to identify and explain the key features of the minimum-energy order by correlating to the underlying flight energy dynamics. It is shown that instead of minimizing the distance, coordination of vertical and horizontal motion to promote aerodynamic efficiency is the key to optimizing energy consumption. In addition, the combination of minimum-energy order planning and energy-optimal trajectory control could achieve energy savings of up to 29.9% over the combined minimum-distance order and a commonly used type of baseline controller.
能量最优多转子运行的三维航路点排序优化
多旋翼飞机实现空中机动是一种具有广泛实际应用的新兴运输方式。最大航程和飞行时间是性能的关键方面,由车辆能源效率控制。研究了多旋翼飞行器的能量最优规划问题,其目的是在三维空间中寻找飞行任务能量消耗最小的航点最优排序。该研究采用了捕获多旋翼第一原理能量动力学的系统模型。研究发现,在大多数情况下(高达95%),能量最优顺序不同于最小距离顺序,这是传统旅行商问题的解决方案。根据任务的距离和其他参数,差异可高达14.9%,平均值为1.6%-3.4%,第90百分位数为3.8%-6.6%。为了验证这些结果,在实际飞行中对三个样本任务进行了测试,结果表明,相对于最小距离顺序,最小能量顺序可以减少3.9%-9.4%的能量成本。这些结果被用来通过与潜在的飞行能量动力学相关联来识别和解释最小能量阶的关键特征。研究结果表明,提高气动效率的垂直运动和水平运动的协调是优化能耗的关键,而不是最小化飞行距离。此外,最小能量阶数规划与能量最优轨迹控制相结合,与最小距离阶数规划和常用的基线控制器相结合,可实现高达29.9%的节能。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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