首页> 外国专利> METHOD FOR INCREASING ACCURACY OF CALIBRATION OF SCALING COEFFICIENTS AND ANGLES OF NON-ORTHOGONALITY OF SENSITIVITY AXES OF SENSOR UNIT OF ANGULAR VELOCITY SENSORS

METHOD FOR INCREASING ACCURACY OF CALIBRATION OF SCALING COEFFICIENTS AND ANGLES OF NON-ORTHOGONALITY OF SENSITIVITY AXES OF SENSOR UNIT OF ANGULAR VELOCITY SENSORS

机译:提高角速度传感器的传感器单元的灵敏度轴的标度系数和非正交性的角度的校准精度的方法

摘要

FIELD: physics.;SUBSTANCE: invention relates to navigation, navigation instruments, testing and calibration, and can be used for calibration of sensors of strapdown inertial systems of orientation and navigation of aircraft, sea, ground and other mobile objects. Method includes initial platform display, static experiment at fixed platform position, rotation with the help of bench equipment in series on at least two non-parallel axes in the calibrated integrated data base basis, during rotation, recording of the integrated data base readings on the linear acceleration sensors (LAS) channel, the angular velocity sensors (AVS) readings, identifying the AVS mathematical model, determining the AVS zero signals, the matrix describing the scale factors, cross-links, developing a calibration process automation program, which includes performing a sequence of rotations and platform slopes at angles in accordance with 6 of the following experiments with duration of time interval with each rotation and inclination of about 3–4 minutes, processing of obtained data, including selection of time interval with duration of about 2-3 minutes with steady angular velocity and inclination angles, calculation of ADC AVS codes average values, differentiation of readings of goniometers and calculation of average values of angular velocities of table platform, calculation of average values of readings of temperature sensors and, using certain algorithms, calculation of calibration coefficients.;EFFECT: technical result is high accuracy of calibration of scaling coefficients and non-orthogonality angles due to invariance to current offsets of zero signals.;1 cl, 3 tbl
机译:技术领域本发明涉及导航,导航仪器,测试和校准,并且可以用于校准飞机,海上,地面和其他移动物体的定向和导航的捷联惯性系统的传感器。方法包括初始平台显示,在固定平台位置进行静态实验,借助台式设备在校准后的集成数据库中至少两个不平行的轴上串联旋转,旋转期间,在平台上记录集成数据库读数线性加速度传感器(LAS)通道,角速度传感器(AVS)读数,识别AVS数学模型,确定AVS零信号,描述比例因子的矩阵,交叉链接,开发校准过程自动化程序,包括执行按照以下实验6中的某个角度的一系列旋转和平台斜率,每次旋转的时间间隔持续时间为3–4分钟,处理获得的数据,包括选择持续时间为2的时间间隔3分钟,具有稳定的角速度和倾斜角,计算ADC AVS代码平均值,并读取读数测角仪的安装,工作台平台角速度平均值的计算,温度传感器读数的平均值的计算以及使用某些算法的校准系数的计算。;效果:技术成果是比例系数校准的高精度和非由于零信号的电流偏移不变而产生的正交角。; 1 cl,3 tbl

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