简介概要

Space range estimate for battery-powered vertical take-off and landing aircraft

来源期刊:中南大学学报(英文版)2015年第9期

论文作者:WANG Bo HOU Zhong-xi GUO Zheng GAO Xian-zhong

文章页码:3338 - 3346

Key words:battery-powered aircraft; vertical take-off and landing; space range; tailsitter

Abstract: A novel method for estimating the space range of battery-powered vertical take-off and landing (VTOL) aircraft is presented. The method is based on flight parameter optimization and numerical iteration. Subsystem models including required thrust, required power and battery discharge models are presented. The problem to be optimized is formulated, and then case study simulation is conducted using the established method for quantitative analysis. Simulation results show that the space range of battery-powered VTOL aircraft in a vertical plane is an oblate curve, which appears horizontally long but vertically short, and the peak point is not located on the vertical climb path. The method and results are confirmed by parameter analysis and validations.

详情信息展示

Space range estimate for battery-powered vertical take-off and landing aircraft

WANG Bo(王波), HOU Zhong-xi(侯中喜), GUO Zheng(郭正), GAO Xian-zhong(高显忠)

(College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China)

Abstract:A novel method for estimating the space range of battery-powered vertical take-off and landing (VTOL) aircraft is presented. The method is based on flight parameter optimization and numerical iteration. Subsystem models including required thrust, required power and battery discharge models are presented. The problem to be optimized is formulated, and then case study simulation is conducted using the established method for quantitative analysis. Simulation results show that the space range of battery-powered VTOL aircraft in a vertical plane is an oblate curve, which appears horizontally long but vertically short, and the peak point is not located on the vertical climb path. The method and results are confirmed by parameter analysis and validations.

Key words:battery-powered aircraft; vertical take-off and landing; space range; tailsitter

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