摘要
利用飞机体轴系下的质点系动力学平衡方程和航迹轴系下的质点动力学平衡方程,将飞机的操纵性、定常性与机动性相结合,给出了飞机水平盘旋/转弯机动的分析方法。对某型飞机的分析结果表明,该方法在飞机设计中具有较高的使用价值。
In this paper, the controllablity, stability and maneuverbility of aircraft are combined in the use of particle dynamics balance equation under an aircraft body and track shaft system. It provides the analysis method of research in aircraft level spiral/turning maneuver, and the analysis of a certain type of aircraft shows that the method has a higher value in aircraft design.
出处
《飞行力学》
CSCD
北大核心
2010年第2期24-27,共4页
Flight Dynamics
关键词
机动性
操纵性
稳定性
盘旋/转弯
maneuverbility
controllablity
stability
spiral/turning
