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kalmanfilt
- 本程序是AR(2)模型进行数据建模，再进行kalman滤波，进行数据去躁处理，尤其用在光纤陀螺上-AR (2) model for data modeling, further Kalman filtering, data processing to impatient, especially with the fiber gyro
navigation
- VC开发，导航程序与串口通信结合，串口连接陀螺采集数据，发给导航程序进行结算-VC, navigation procedures and integrate serial communication, serial connectivity gyro data collection, to navigation procedures for clearing
Gyro Dynamics Simulation
- 陀螺動態模擬程序 使用錐形體代表陀螺
InertialNavigation
- 捷联导航相关知识，陀螺，及速度及惯性敏感器件和测试、补偿标定技术以及捷联系统算法的相关知识-Strapdown navigation knowledge, gyro, and speed and inertia-sensitive devices and tests, calibration and compensation algorithms SINS knowledge
StrapdownDataGenerator
- 捷联惯导系统的陀螺及加速度计数据发生器。-SINS gyro and accelerometer data generator
Strapdown
- 一、数据说明： 1：惯导系统为指北方位的捷连系统。初始经度为116.344695283度、纬度为39.975172度,高度h为30米。 初速度为v0=[0.000048637 0.000206947 0.007106781]，飞行高度不变。 2：jlfw中为600秒的数据，陀螺仪和加速度计采样周期分别为为1/80秒和1/80秒。 3：初始姿态角为[0.120992605 0.010445947 91.637207]（俯仰，横滚，航向,单位为度）, jlfw中保存的为比力信
Gyro_dynamics_simulation_MATLAB
- 陀螺运动的仿真程序，动力学仿真和动画同时表示 陀螺在重力下以适当的初始速度落地的仿真结果-Gyro movement simulation program, dynamic simulation and animation at the same time that the top of the gravity of the initial velocity to the appropriate landing simulation results
tiltsensor
- tilt sensor, gyro, tilt sensor, gyro,
tuoluobiaodinggongshi
- 适用于大部分类型的陀螺数据处理的matalb程序,包括标度因数,零偏,补偿等信息-Applicable to most types of gyro data processing matalb procedures, including scale factor, bias, compensation and other information
simutrack
- 陀螺加表数据发生器，可以自动生成足够数量的数据。-Gyro Add table data generator can automatically generate a sufficient number of data.
navi_test
- 惯性导航的MATLAB算法，根据陀螺与加表的值计算姿态-MATLAB inertial navigation algorithm, based on gyro and attitude add value table
robot.tar
- robot-gyro and gsensor-kalman filter-state space
es
- 恒流源的陀螺仪测温丝电阻测量电路的设计-Gyro temperature constant current source circuit wire resistance measurement
Nav
- 利用陀螺仪和加表的输出进行惯导结算，得到飞机的位置，速度，姿态角-Use of gyro inertial navigation and processing the output of clearing the table to get the aircraft position, velocity, attitude angle
thegyroscopeoutputdata-processing
- 对采集的陀螺数据进行处理 滤除陀螺输出的随即漂移-Collected data for processing filtered gyro gyro output drift immediately
44
- 用于飞行器自动控制的算法计算， 融合三轴加速度计和三轴陀螺的数据融合计算，得出飞行姿态-For aircraft automatic control algorithm, integrated three-axis accelerometer and three-axis gyro data fusion calculations, flight attitude
cd4ef1.ZIP
- 三轴转台误差对陀螺仪标定精确度的影响Three axis turntable error of gyro calibration accuracy influence-Three axis turntable error of gyro calibration accuracy influence
gyro_allan_t
- 自己编的Allan方差计算函数，经过了反复测试。输入为陀螺频率数据和采样时间间隔。可以自定义只计算部分相关时间对应方差值。-Allan variance calculation function, after repeated tests. Input is the gyro frequency data and the sampling time interval. The part of the correlation time corresponding to the variance C
gyro_hdmvar_t
- 自己编的哈达玛方差计算函数，经过了反复测试。输入为陀螺频率数据和采样时间间隔。-Hadamard variance calculation function, after repeated tests. The input is gyro frequency data and the sampling time interval.
Gyro-nonlinear-test
- 计算光纤陀螺的非线性度，并且绘制出不同速率对应的非线性度曲线。-Calculation of the non-linearity of the optical fiber gyro, and draw out the different rates corresponding to the non-linearity curve.