Invention Grant
US09086284B2 Method for automatically managing a pitch rate gyroscope mounted on a flying device 有权
自动管理安装在飞行装置上的俯仰率陀螺仪的​​方法

Method for automatically managing a pitch rate gyroscope mounted on a flying device
Abstract:
The invention relates to a flying device (1), in particular an air missile, which is of the inertial navigation type, which is rotatable and includes a pitch rate gyroscope (2), wherein said device also comprises automatic control means (8) for rotating same about the longitudinal axis (3) thereof, regularly alternating the direction of rotation, so as to cancel the effect of the scale factor of the pitch rate gyroscope (2), in addition to correcting ordinary drifts.
Information query
Patent Agency Ranking
0/0