摘要
文中应用分歧与突变理论法建立了翼伞系统飞行稳定性分析的方法。该方法非常程序化,便于应用计算机求解,通过计算结果的图形显示,可非常直观地了解翼伞系统设计参数对系统稳定性的影响,给出翼伞系统的全局稳定性分析结果,为翼伞设计人员提供必要的设计参考数据。
The bifurcation analysis and catastrophe theory methodology is used here t?find ways to analyze the stability of parafoil system.Influence of the system design parameters on stability can be visually observed from graphically displayed results computed with the help of this highly Programmed method and qualitative analytical results of global stability of parafoil system can be provided as essential reference data for designers.
出处
《航天返回与遥感》
1995年第4期1-6,共6页
Spacecraft Recovery & Remote Sensing
