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飞行器动态滑翔的受力平衡状态

单上求 侯中喜 王鹏 郭正

国防科技大学学报2017,Vol.39Issue(4):15-20,6.
国防科技大学学报2017,Vol.39Issue(4):15-20,6.DOI:10.11887/j.cn.201704003

飞行器动态滑翔的受力平衡状态

Force balance in dynamic soaring of aerial vehicle

单上求 1侯中喜 1王鹏 1郭正1

作者信息

  • 1. 国防科技大学 航天科学与工程学院,湖南 长沙 410073
  • 折叠

摘要

Abstract

To clarify the physical essential, a perspective of force balance to dynamic soaring was put forward.Equilibrium equations were derived according to physical laws.The solution of the equations solved mathematically formed a curve.Simulations of the curve were made in the cases of an albatross and an unmanned air vehicle in different wind gradients for instances.The results of analysis and simulation indicate that the curve is the velocity set that satisfies the equilibrium equations;the curve consists of a climbing branch and a diving one;the climbing branch exists only if the gradient is sufficiently large, and it is critical to dynamic soaring.

关键词

动态滑翔/无动力飞行/风梯度/受力平衡/无人机

Key words

dynamic soaring/effortless flight/wind gradient/force balance/unmanned air vehicle

分类

航空航天

引用本文复制引用

单上求,侯中喜,王鹏,郭正..飞行器动态滑翔的受力平衡状态[J].国防科技大学学报,2017,39(4):15-20,6.

基金项目

国家863计划资助项目(2014AA7054035) (2014AA7054035)

国防科技大学学报

OA北大核心CSCDCSTPCD

1001-2486

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