建立了可用于现代火控计算机的火控弹道权函数法模型。
Presents a weighted function model for the flight traJectory of projectiles, oriented for applications with computers in modern fire control systems.
建立了再入机动弹道数学模型，给出了气动力系数为速度、迎角、高度的函数拟合式，进行了最佳再入机动弹道设计和仿真计算。
The mathematical model of reentry maneuvering trajectory is established. The fitting expression of aerodynamic coefficient function on velocity, attack of Angle and altitude is presented.
弹道修正弹； 灵敏度函数； 辨识； 最优控制； 舵机。
Trajectory correction projectile; Sensitivity function; Identification; Optimal control; Actuator.
应用推荐