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低空航路线形设计要素对飞行器能耗的影响分析

马涛 董政显 唐樊龙 王宁 牟天昊 范剑伟

东南大学学报(自然科学版)2026,Vol.56Issue(6):873-884,12.
东南大学学报(自然科学版)2026,Vol.56Issue(6):873-884,12.DOI:10.3969/j.issn.1001-0505.2026.06.009

低空航路线形设计要素对飞行器能耗的影响分析

Analysis of the impact of low-altitude route geometry design elements on aircraft energy consumption

马涛 1董政显 1唐樊龙 2王宁 3牟天昊 1范剑伟4

作者信息

  • 1. 东南大学交通学院,南京 211189
  • 2. 东南大学交通学院,南京 211189||金陵科技学院网络与通信学院,南京 211199
  • 3. 东南大学交通学院,南京 211189||南京林业大学土木工程学院,南京 210037
  • 4. 金陵科技学院机电工程学院,南京 211199
  • 折叠

摘要

Abstract

To guide the design of energy-efficient low-altitude routes,this paper proposes a methodological framework for calculating the operating energy consumption of low-altitude routes during design phase.This framework accounts for the impact of low-altitude route design elements on aircraft operating speeds.Further-more,taking multi-rotor UAVs as an example,the framework was used to analyze the influence of design ele-ments and their combinations within route units on the operating energy consumption of UAVs.The results in-dicate that route length,horizontal curve radius,slope angle,vertical curve radius,and the tangent angles at the start and end points of the vertical curve are the primary design elements affecting energy consumption.Fi-nally,based on calculation results,operating energy consumption assessment formulas for low-altitude routes were regressed,with the design elements as independent variables.The regression formula demonstrates high fitting accuracy.

关键词

节能化低空航路/低空航路运行能耗计算框架/多旋翼无人机/运行能耗评估公式

Key words

energy-efficient low-altitude route/low-altitude route operating energy consumption calculation framework/multi-rotor UAVs/operating energy consumption evaluation formula

分类

航空航天

引用本文复制引用

马涛,董政显,唐樊龙,王宁,牟天昊,范剑伟..低空航路线形设计要素对飞行器能耗的影响分析[J].东南大学学报(自然科学版),2026,56(6):873-884,12.

基金项目

国家自然科学基金资助项目(52378445) (52378445)

江苏省自然科学基金青年基金资助项目(BK20251267). (BK20251267)

东南大学学报(自然科学版)

1001-0505

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