摘要
介绍了数字式导弹自动驾驶仪控制回路分析与设计的三种方法 ,即连续化方法、离散化方法和连续 /离散混合系统设计方法 .讨论了这三种设计方法各自的优缺点及在设计过程中需要注意的问题 ,并通过一个具体的仿真实例验证了所得出的结论 .
The three methods of analysis and design for control loop of missile digital autopilot are introduced,viz.continuum method,discreteness method and hybrid systems method.The advantage and disadvantage of each method and the problems needs to pay attention to in the course of design are discussed.At last,a simulation example is given to verify the conclusions.
出处
《战术导弹技术》
2003年第1期59-65,共7页
Tactical Missile Technology