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- 一些姿态结算的好程序，大家共同分享，共同进步，共同提高-Abstract：Aim ing at determining the satellite attitude precisely，the gyros bias and m isa l
InertialADXLreadout
- This program implements all aspects of readout of ADXL accelerometer in Delphi. It enables plotting and checking of output of typical ADXL 202 accelerometer. You can set RS via ini file and add more functionality Do not
MikroQuadAero_v2.1
- This project will use the Arduino Diecimila as the hardware platform to control a quadrocopter. Software coding will be done in the Arduino environment. The primary goal for this quadrocopter will be to create a low cost
EKF_MEMS
- 姿态信息是飞行控制中最关键的参数之一,因此姿态测量成为飞行控制系统首要解决的问题。利用多MEMS传感器研制了一种微型姿态测量系统。利用三轴MEMS加速度计和三轴MEMS陀螺数据,由方向余弦矩阵的姿态表示形式推导了扩展Kalman滤波方程,解算出飞行器的俯仰角和横滚角 设计专家系统判断飞行器的运动状态,并根据该状态调整滤波算法中的测量噪声矩阵,使系统可同时满足静态情况和动态情况的使用 利用空速和高度数据对俯仰角进行修正,利用GPS解算航向
gyro_EKF
- Aiming at determining the satellite attitude precisely，the gyros bias and m isa lignment were compensated in time by using the quaternion of star-sensor and extended Kalm an filter．The related module of the filter was de
Direct
- dBasic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establi
Direct_C_Noise
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establish
GEN
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establish
Indirect_Cancel
- Basic principles of the strapdown inertial navigation system (SINS) using the outputs of strapdown gyros and accelerometers are explained, and the main equations are described. A mathematical model of SINS is establish
new_strapdown
- Abstract—A new calibration procedure was proposed for strap down inertial measurement unit (IMU) in a body reference fr a me which was independent of the turntable. The proposed methodology required no precise mech
GyroAndAccDataReader
- 陀螺仪数据采集程序 采用转换串口采集数据后直接传到MATLAB中，适用于单轴陀螺仪数据快速采集与标定-the programme to get the datas from gyros
speed-control-
- 采用变速控制力矩陀螺的航天器自适应姿态跟踪和稳定控制研究-Using variable speed control moment gyros Spacecraft Adaptive Attitude Tracking Study and stability control
speed-control-
- 采用变速控制力矩陀螺的航天器自适应姿态跟踪和稳定控制研究，编程学习源码，很好的学习资料。-With variable speed control moment gyros Adaptive Spacecraft Attitude Tracking Study and stability control, programming, learning code, good learning materials.
gyro-and-acce-simulink
- this a simulink file about gyros and acceleration ingration
Allan_Variance
- allan 方差（阿伦方差）是David AIlan于1966年提出的，最初该方法是用于分析振荡器的相位和频率不稳定性，高稳定度振荡器的频率稳定度的时域表征目前均采用Allan方差。由于陀螺等惯性传感器本身也具有振荡器的特征，因此该方法随后被广泛应用于各种惯性传感器的随机误差辨识中。(Allan variance (Allen variance) was proposed by David Allan in 1966. Initiall