摘要
为了更有效地对导弹制导与控制技术进行研究,设计了一种以仿真技术和弹上计算机相结合的测试系统。通过仿真计算机输出相应的加速度脉冲给弹上计算机,弹上计算机输出反馈信号给仿真计算机,从而实现测试系统的闭环工作。该测试系统能同时考察弹上多种硬件设备及飞行控制程序的工作状态,对优化制导与控制方法有较大的帮助。
A test system based simulation method and computer of the missile is designed for efficient research on missile＇ s control and guidance method. The simulation computer sends acceleration impulse to computer of the missile and the computer of the missile sends feedback signal to the simulation computer, which realizes the system work in the closed loop. This system can optimize missile＇ s control and guidance method, beeause it can test many kinds of missile units and program of missile control.
出处
《飞行力学》
CSCD
北大核心
2008年第5期75-77,81,共4页
Flight Dynamics
关键词
导弹
制导
半实物仿真
missile
control and guidance
hardware-in-the-loop simulation
