基于某型防空导弹飞行仿真的控制机制研究

Study of Control Mechanism Based on One Antiaircraft Missile Flying Simulation

在某型防空导弹虚拟发射飞行系统仿真中 ,能否准确地对导弹发射过程进行控制是实现该系统功能的关键。另外 ,该系统还需在导弹飞行的关键点处向主控台传递消息。该文依托Windows 98操作系统 ,通过网络交换器与主控台相连 ,利用Winsock实现主控台命令的传输。最后 ,通过VC ++编程实现了图形机响应主控台的命令完成导弹的发射、导弹击中目标或自毁以及当导弹发射后导弹能够命中目标或进入自毁程序等关键点处向主控台发送消息等功能。

In an antiaircraft missile flying simulation system, it is the key that whether the process of missile launch can be controlled well and truly. In addition, this system even requires transferring message to main control platform at pivotal points of missile flying. In this paper, the graphic computer relying on Windows 98 operating system and Hub joins to main control platform. Then, using Winsock, we realize the transmission of main control' s order. Finally, we apply VC++ to program and realize the function of graphic computer responding to main control platform's order and sending message to main control platform.