The present model is capable of estimating aerodynamiccoefficient ratios including the important static stability margin.
本模型可精确估计气动系数比，其中包括重要的静稳定度。
2
The aerodynamiccoefficient varies with dynamic pressures always linearly, no matter what a rigid aerodynamic force may be linear or non-linear.
不论刚体气动力为线性还是非线性，气动力系数随动压变化的趋势均呈线性。
3
The mathematical model of reentry maneuvering trajectory is established. The fitting expression of aerodynamiccoefficient function on velocity, attack of Angle and altitude is presented.