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stepbystepmotorcontrol
- 单片机采集陀螺信号，并控制步进电机与陀螺相反的方向转动-Single-chip gyroscope signal acquisition, and control the stepper motor in the opposite direction with the gyro rotation
Simp_Unscented
- 抖动的存在，陀螺输出脉冲数在正负200之间跳动；其频谱表现为在抖动频率处的一个能量非常高（14000）的谱线；500～1000赫兹之间也有40左右的能量，表明陀螺输出存在一定的高频噪-The existence of jitter, gyro output pulses beating in between plus or minus 200 the performance of its spectrum in the frequen
MicrostoneGyroSensor
- 高速陀螺数据手册 奥巴马已经限制出口中国的芯片 开发导弹需要使用到的技术-High-speed gyro data sheet limits of Obama' s chip exports to China need to develop missile technology
friction
- 本文以某型陀螺漂移测试转台控制系统设计实现为背景，针对系统中存在的非线性摩擦影响，着眼于包括摩擦在内的转台控制系统的建模、摩擦影响分析以及摩擦补偿问题，从理论上进行了分析和研究，并对提出的补偿方法进行了计算机仿真验证。-In this paper, a certain type of gyro drift test turntable control system design to achieve as the background
Navigation_integration_algorithm
- 最近在弄陀螺稳定，得到这篇很经典的资料，江南航天集团的。捷联式惯性导航积分算法。很稀罕的。-Get gyro stabilized recently received information of this classic, Jiangnan Aerospace Group. Strapdown inertial navigation integration algorithm. Very rare for.
SINGLE255
- 双轴陀螺芯片ADIS16255单片机控制，SPI读并通过串口输出-Dual-axis gyro chip ADIS16255 SCM control, SPI read through the serial port output
ogl_vertex_array_range
- 此为关于陀螺仪的一个MATLAB程序。经过仿真得到陀螺仪的运动状况-This is on a MATLAB program gyroscope. The simulation to be the movement of gyroscope
tuoluoti
- 哈工大的陀螺仪原理，讲述了微机械陀螺仪，挠性陀螺，激光陀螺等！-HIT gyroscope principle described micromachined gyroscope, flexible gyro and laser gyro and so on!
coning-algorithm
- coning_atti:基于角速率输入的1～5子样等效转动矢量姿态仿真程序。 coning_atti_imu_error：等效转动矢量法仿真程序，包含1～4子样的各种等效转动矢量法，以读文件形式读取IMU输出参数，IMU参数由wnbb_error事先生成。 wnbb_error:用来产生带IMU误差的标准圆锥运动Gyro输出参数。 -coning_atti: Based on the input angular r
AttitudeAlgorithmwithIncrementalAngleofRLGSINS
- 摘要针对激光陀螺的零偏受温度影响较大，为提高陀螺精度，研究了二频机抖激光陀螺抖动频率与温度之间的关系。-Abstract The laser gyro bias affected by temperature, in order to enhance the precision gyroscope to study mechanically dithered laser gyro dither frequency and tempera
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
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
gyrocompensate
- temperature compensation method for gyro
neuranetworktemperature
- neural network based temperature error compensation for gyro
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.
alan
- ALLAN方差是阿兰发明的，在惯性导航中应用及其广泛，这篇论文在陀螺数据处理方面具有很好的方法-ALLAN Allan variance is the invention, in the inertial navigation system and its broad application, this thesis has a very good gyro data processing methods
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
nordic-nRF24LE1
- Nordic Semiconductor，nRF24LE1无线语音门铃系统-Nordic Semiconductor, nRF24LE1 doorbell system wireless voice
Attitude_Kalman_gom
- 卡尔曼滤波器，具体组合为轨道罗盘+磁强计+速率陀螺，具体物理含义请见附件中的注释，航天人可以一目了然-Kalman filter, the specific combination of orbital compass+ magnetometer+ rate gyro, the specific physical meaning, please see attached comments in the space one can at
C_newtyle
- 航天常用姿态确定敏感器组合，太阳敏感器+速率陀螺+轨道罗盘，具体数据含义请参考章仁为的<《卫星姿态控制》>-Spacecraft attitude determination sensors commonly used in combination, sun sensor+ rate gyro compass+ tracks, the meaning of specific data please refer to Chap