首页> 外国专利> METHOD OF ESTIMATING ERRORS AND CONTROLLING RAW INFORMATION SENSORS IN GIMBALLESS INERTIAL NAVIGATION SYSTEM IN GROUND CONDITIONS AND APPARATUS THEREFOR

METHOD OF ESTIMATING ERRORS AND CONTROLLING RAW INFORMATION SENSORS IN GIMBALLESS INERTIAL NAVIGATION SYSTEM IN GROUND CONDITIONS AND APPARATUS THEREFOR

机译:地面条件下无惯性惯性导航系统中误差估计和原始信息传感器的控制方法及装置

摘要

FIELD: physics, navigation.;SUBSTANCE: invention relates to instrument-making and can be used in processes for controlling raw information sensors in a gimballess inertial navigation system (GINS) in ground conditions. Error estimation and control of raw information sensors in a GINS is carried out by mounting the GINS on a platform with a base and carrying out initial alignment of the GINS, followed by conversion thereof to self-contained operating mode. In said mode, the GINS is successively turned by certain banking and pitch angles, followed by pre-start check of errors of the GINS. The apparatus for implementing the method consists of a base 1 on which a platform 2 is placed for mounting the GINS to be inspected. The base 1 is in the form of a rotating frame, the rotational axis 5 of which is perpendicular to the rotational axis 7 of the rotating platform 2. On the rotational axes 5 and 7 of the base 1 and the platform 2, there are drives for setting the banking and pitch angles of the inspected GINS.;EFFECT: increased reliability.;2 cl, 1 dwg
机译:技术领域本发明涉及仪器制造,并且可以用于在地面条件下控制无万向节惯性导航系统(GINS)中的原始信息传感器的过程。通过将GINS安装在带有底座的平台上并进行GINS的初始对准,然后将其转换为独立的操作模式,可以对GINS中的原始信息传感器进行错误估计和控制。在所述模式下,GINS依次旋转一定的倾斜角和俯仰角,然后对GINS的误差进行预启动检查。用于实施该方法的设备包括基座1,在基座1上放置平台2以安装要检查的GINS。基座1为旋转框架的形式,其旋转轴5垂直于旋转平台2的旋转轴7。在基座1和平台2的旋转轴5和7上有驱动器。用于设置检查的GINS的倾斜角和俯仰角。;效果:提高可靠性。; 2 cl,1 dwg

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