摘要
结合一种由阻尼陀螺和加速度计组成的传统的导弹自动驾驶仪,通过对加速度计测角速度原理的分析,提出了两种适用于工程实际的在俯仰和航向两通道实现无陀螺数字式自动驾驶仪的设计方案,并通过应用实例证明了这两种方案的可行性。
A kind of traditional missile's autopilot composed of rate gyro and accelerometer and measuring angle principle of accelerometer are analyzed, then two design proposal of digital autopilot with nongyroscope but accelerometer combination in pitch and yaw channel are proposed, which are suitable to engineering application. Finally, an applied example is given.
出处
《战术导弹技术》
1998年第4期41-46,共6页
Tactical Missile Technology
