论文部分内容阅读
航天飞机在大气层中的飞行稳定性分析属于非线性动力学系统范畴.通过分析其运动方程组的导算子矩阵,得出了航天飞机高机动大攻角飞行的稳定性判据,同时指出,BATCM分析方法是航天飞机飞行稳定及控制分析与设计的有效途径.
The stability analysis of space shuttle in the atmosphere belongs to the category of nonlinear dynamical system. By analyzing the guide operator matrix of its equations of motion, the stability criterion of the space shuttle at high maneuvering attack angle is obtained. At the same time, The BATCM method is an effective approach to the stability and control analysis and design of a space shuttle.