低空航路线形设计要素对飞行器能耗的影响分析OA
Analysis of the impact of low-altitude route geometry design elements on aircraft energy consumption
为指导节能化低空航路设计,本文提出一种在设计阶段计算低空航路运行能耗的方法框架.该框架考虑了低空航路设计要素对飞行器运行速度的影响.同时,以多旋翼无人机为例,基于该框架系统分析了不同航路单元中各设计要素及其组合对无人机运行能耗的影响规律.结果表明,航路长度、圆曲线半径、斜坡角度、竖曲线半径、竖曲线起终点切线角度是影响低空航路运行能耗的主要设计要素.最后,基于框架的计算结果,以设计要素为自变量回归了方便设计人员直接使用的低空航路运行能耗评估公式.该回归公式具有较高的拟合精度.
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.
马涛;董政显;唐樊龙;王宁;牟天昊;范剑伟
东南大学交通学院,南京 211189东南大学交通学院,南京 211189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东南大学交通学院,南京 211189金陵科技学院机电工程学院,南京 211199
航空航天
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
energy-efficient low-altitude routelow-altitude route operating energy consumption calculation frameworkmulti-rotor UAVsoperating energy consumption evaluation formula
《东南大学学报(自然科学版)》 2026 (6)
873-884,12
国家自然科学基金资助项目(52378445)江苏省自然科学基金青年基金资助项目(BK20251267).
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