说明：  对某飞行器的全空域飞行弹道进行了仿真研究.建立了飞行器空间运动的数学模型，应用“牛顿插值多项式法”对气动力参数进行了辨识，用C语言编制了仿真程序，并给出了仿真结果及分析。
(Of a vehicle-wide airspace simulation trajectory. Established the aircraft mathematical model of space motion, application, Newton interpolation polynomial method on the aerodynamic parameters identification, use of C language compiled simulation program, and to out the simulation results and analysis.)