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微小型垂直起降飞行器悬停时往往采用螺旋桨滑流内舵面偏转进行姿态控制,但容易出现操纵力矩不足的问题。本文针对这一问题对微小型静推力状态螺旋桨与带舵面机翼的组合体进行了系统性的实验。通过对实验数据分析,本文指出通过优选螺旋桨几何参数可以改善操纵特性,并得出带舵面机翼不同构型对操纵特性影响的一系列结论,为如何改善此类飞行器悬停时的操纵特性提供了设计参考。
Micro vertical VTOL aircraft hovering often use propeller slip surface rudder deflection attitude control, but prone to lack of maneuvering torque problems. In this paper, a systematic experiment on the combination of a miniature static thrust propeller and a wing with a control surface is carried out in response to this problem. Through the analysis of the experimental data, this paper points out that the propeller geometry parameters can improve the steering characteristics, and draw a series of conclusions about the different configurations of the control wing with the rudder wing. How to improve the maneuvering characteristics of the hovering vehicle Provides a design reference.