前言确定有翼导弹稳定性的合理范围,是设计有翼导弹的重要课题之一。本文研究有翼导弹弹体的稳定性与导弹稳定系统的稳定性、动态品质以及机动性(以弹道倾角角速度的稳态值为指标)之间的相互关系,进而应用界线法,以确定导弹弹体稳定性及自动器参数的合理范围。由于 Preface Determining the reasonable range of the stability of a winged missile is one of the important topics in the design of a winged missile. In this paper, we study the relationship between the stability of the aero-missile missile body and the stability, dynamic quality and mobility of the missile stability system (using the steady-state value of ballistic inclination angular velocity as an index), and then apply the boundary line method to determine the missile bombs Body stability and automatic parameters of a reasonable range. due to