本仿真系统提供了一个对导弹进行精确制导打击飞行目标(F14)的仿真平台。系统首先仿真雷达获取飞行目标的飞行信息，包括飞行速度与飞行姿态；接着导弹基于飞行接近的追踪算法产生当前时刻导弹的速度与姿态；整个系统的构成包括有：F14战斗机3D模型，空空导弹3D模型；仿真雷达站。-This simulation system provides a to precision-guided missiles hit target (F14) flight simulation platform.Simulat

生成纵横向四阶方程，计算特征根，传递函数等，给出波特图及尼科尔斯图。- SURVEY is set up to make calculations based on the 12 x 12 Fmodel and 12 x 7 Gmodel produced by FLIGHT, with the generic business jet model trimmed for flight at V = 102 m/s and h = 3,050 m. The flags are set to ge

IMC-PID是利用内模控制原理来对PID参数进行计算，包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角，加入重复控制。- The IMC- PID is using the internal model control principle for PID parameters is calculated, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle