摘要
分析了抖动式激光陀螺经过零速率点引起的误差特征。根据此误差特征 。
The characteristic of the error introduced when the gyro input rate is cycled through the lock in zone is analyzed.According to the characteristic,the dependence of the error on the parameters of the gyro is systematically derived.A brief discussion is given.
出处
《宇航学报》
EI
CSCD
北大核心
2000年第3期58-63,共6页
Journal of Astronautics