交通运输系统工程与信息 ›› 2026, Vol. 26 ›› Issue (3): 348-359.DOI: 10.16097/j.cnki.1009-6744.2026.03.031

• 系统工程理论与方法 • 上一篇    下一篇

融合速度障碍与人工势场法的电动垂直起降飞行器路径规划

唐立*1a,1b ,何彪1a,1b ,唐昕琛1c ,王焜2   

  1. 1. 西华大学,a.汽车与交通学院,b.智能空地融合载具及管控教育部工程研究中心,c.机械工程学院,成都610039; 2. 香港理工大学,工业及系统工程学系,香港999077
  • 收稿日期:2025-12-15 修回日期:2026-03-23 接受日期:2026-03-30 出版日期:2026-06-25 发布日期:2026-06-23
  • 作者简介:唐立(1988—),女,四川遂宁人,副教授,博士。
  • 基金资助:
    智能空地融合载具及管控教育部工程研究中心开放课题(ZNKD2025-01);国家自然科学基金(52102384)。

Path Planning of Electric Vertical Take-off and Landing Aircraft Considering Velocity Obstacle and Artificial Potential Field

TANG Li*1a,1b, HE Biao1a,1b, TANG Xinchen1c, WANG Kun2   

  1. 1a. School of Automobile and Transportation, 1b. Engineering Research Center of Intelligent Space Ground Integration Vehicle and Control, Ministry of Education, 1c. School of Mechanical Engineering, Xihua University, Chengdu 610039, China; 2. Department of Industrial and Systems Engineering, the Hong Kong Polytechnic University, Hong Kong 999077, China
  • Received:2025-12-15 Revised:2026-03-23 Accepted:2026-03-30 Online:2026-06-25 Published:2026-06-23
  • Supported by:
    Open Research Subject o fEngineering Research Center of Intelligent Air-Ground Integration Vehicle and Control (Xihua University), Ministry of Education (ZNKD2025-01);National Natural Science Foundation of China (52102384)。

摘要: 针对现有电动垂直起降飞行器路径规划算法较多以全局静态规划为主,难以在复杂低空场景中对动态障碍物(例如其他飞行器、鸟类和空飘物等)进行实时响应,进而造成实时避障能力方面的不足,本文融合速度障碍法与人工势场法,构建面向复杂三维低空环境的电动垂直起降飞行器避障路径规划算法。该算法在规划过程中综合考虑飞行器动力学约束与障碍物运动特性,通过速度障碍法计算飞行器和障碍物的相对速度和角度等参数,筛选冲突避障区域,并利用人工势场模型动态调节吸引力与斥力函数,引导飞行器逐步返回航路,实现全局路径优化与局部避障的统一。以四川省成都市天府新区部分区域为背景,开展1∶10缩比仿真试验,构建真实地理约束下的常规开阔空域与受限狭窄空间两类场景,并设置高密度障碍物场景检验算法在高复杂度条件下的适应性与鲁棒性。试验结果表明:在常规开阔场景中,所提算法与速度障碍法和人工势场法相比,迭代次数分别减小24.7%和20.2%,路径长度分别缩短19.8%和30.4%;在受限狭窄空间与高密度障碍物场景下,该算法有效克服传统方法易引发的局部震荡与过度绕行缺陷,并大幅降低飞行器的累积偏航角,显著提升航迹的平滑度与物理可飞性。

关键词: 城市交通, 路径规划, 速度障碍-人工势场法, 电动垂直起降飞行器, 低空经济

Abstract: Existing path planning algorithms for electric vertical take-off and landing aircraft predominantly use global static planning, and have difficulties to respond in real-time to dynamic obstacles (such as other aircraft, birds, or airborne debris) within complex low-altitude environments. This limitation impedes their real-time obstacle avoidance capabilities. This paper integrates the velocity obstacle method with the artificial potential field approach to develop an obstacle avoidance path planning algorithm for electric vertical take-off and landing aircraft operating in complex three-dimensional low-altitude environments. This algorithm considers both the aircraft's dynamic constraints and the motion characteristics of obstacles during the planning process. It uses the velocity obstacle method to calculate parameters such as the relative velocity and angle between the aircraft and obstacles, thereby identifying conflict avoidance zones. Furthermore, it utilizes an artificial potential field model to dynamically adjust attraction and repulsion functions, guiding the aircraft to progressively return to its flight path. This approach achieves a unified solution for global path optimization and local obstacle avoidance. Using parts of Tianfu New Area in Chengdu city as the setting, the study conducted 1∶10 scale simulation experiments to analyze two scenarios—conventional open airspace and confined narrow spaces— under real-world geographical constraints. Additionally, a high-density obstacle scenario was established to test the algorithm's adaptability and robustness under highly complex conditions. The experimental results indicate that, in conventional open-space scenarios, the proposed algorithm reduces the number of iterations by 24.7% and shortens the path length by 19.8% compared to the velocity-obstacle method. Compared to the artificial potential field method, it reduces the number of iterations by 20.2% and shortens the path length by 30.4%. In confined spaces and high-density obstacle scenarios, the algorithm effectively overcomes the local oscillations and excessive detours commonly caused by traditional methods, and significantly reduces the cumulative yaw angle of the aircraft and improves the smoothness and physical flyability of the flight path.

Key words: urban transportation, path planning, velocity obstacle-artificial potential field method, electric vertical take-off and landing aircraft, low-altitude economy

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