摘要
根据陀螺的动力学方程,从陀螺设计中的重要参数——内、外框架组件的等惯量约束条件和振动灵敏度等角度,探讨了检测质量对陀螺性能的影响,为微机械框架振动陀螺的设计提供了理论依据。
The impact proof mass on the gyros performance is discussed on the basis of microgyro dynamic equation and several important parameters in the design of micromechanical vibrating gyros, including equivalent moment of inertia constraint conditions in the inner and outer gimbals, sensitivity, etc . This study will lay foundation for the gyros design in the near future.
出处
《航空学报》
EI
CAS
CSCD
北大核心
1997年第4期489-492,共4页
Acta Aeronautica et Astronautica Sinica
关键词
微机械框架
陀螺
检测质量
等惯量约束
微陀螺
micromechanical gimbal vibrating gyroscope, proof mass, sensitivity, equivalent moment of inertia constraint conditions