An eVTOL energy-saving path planning method considering dynamic meteorological constraints

By constructing an eVTOL energy-saving path planning method that considers dynamic weather constraints, predicting the range of weather blockages and quantifying passability, and combining hovering and detour strategies, the problem of energy consumption prediction and the impact of weather restrictions in existing technologies is solved, achieving energy-optimal path planning and improving the range and robustness of eVTOL path planning.

CN122408770APending Publication Date: 2026-07-17GUANGXI UNIV

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
GUANGXI UNIV
Filing Date
2026-04-15
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing eVTOL energy-saving path planning technology does not fully consider the differences in rotor hovering energy consumption, air resistance, speed and altitude, and fails to effectively cope with the impact of temporary weather restrictions in urban low-altitude flight, resulting in discrepancies between energy consumption prediction and actual energy consumption, making it difficult to obtain the optimal solution.

Method used

By constructing an energy-saving path planning method that considers dynamic meteorological constraints, the spatiotemporal impact range of meteorological blockages is predicted, the passability of blocked flight segments is quantified, and the optimal energy consumption decision is made between hovering and detouring. The hovering and detouring strategies are constructed, and the scheme with the minimum total energy consumption is selected.

Benefits of technology

It significantly reduces energy loss of eVTOL under microweather and temporary weather restrictions, and improves range and route planning robustness.

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Abstract

本发明涉及城市空中交通中低空飞行安全与航迹规划技术领域,具体为一种考虑动态气象约束的eVTOL节能路径规划方法,步骤一、建立三维禁飞体,形成基础空域图;步骤二、建立对应阶段的能耗计算公式;步骤三、构建航段能耗加权拓扑图;步骤四、构建含阻断范围、高度、时间窗、属性的气象阻断区域以及生成航段解除概率函数;步骤五、判断是否可通行;步骤六、若不可通行,构建悬停待飞策略与航路绕行策略;步骤七、以总能耗最小为准则,从两类策略中选择最优方案,输出对应轨迹及总能耗评估结果。本发明实现了能耗意义下的最优路径规划;实现了对航段“暂时不可通行”情形的可通过性量化评估;显著降低了能耗损失。
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