搜索资源列表
SIM_IMU
- 惯性导航算法,实现陀螺仪的仿真,用于陀螺选型-inertial navigation algorithm, and the simulation gyroscope for gyro Selection
Kalman_sgm
- 卡尔曼滤波器，敏感器组合形式为数字太阳敏感器+磁强计+速率陀螺，具体的参数物理含义请见文件中的注释，航天人依旧一目了然-Kalman filter sensor combinations for the digital sun sensor+ magnetometer+ rate gyroscope, specifically the physical meaning of parameters see comments in the file, astronauts still at a gl
GY_80_9axi_BMP085
- 陀螺及加速度计和压力计组合成的方位解算软件，51单片机实现的解算。方位较为准确。-The azimuth gyroscope and accelerometer and manometer combined into solver software, to 51 MCU solver. The orientation is more accurate.
STIM202
- 该文档描述了STIM202三轴陀螺仪的特性特征，在角度测量方面比较精确-This document describes the STIM202 axis gyroscope characteristic feature accurate angle measurement
kalman_wwh
- 实现GPS/INS组合导航解算位置、速度、航向等参数。输入数据：东向位置、北向位置、航向角（度）、gps速度、陀螺仪角速度、里程计脉冲数-Implement integrated GPS/INS navigation solution position, speed, course and other parameters. Input data: east position, north position, heading angle (degrees), gps speed, angular
IMU
- 采用加速度计和陀螺仪互补滤波获得载体三维姿态。-Using accelerometer and gyroscope carrier complementary filter to get 3 d pose.
duoziyang
- 由飞机陀螺仪所给出的数据，分别通过单子样，双子样，四子样方法进行飞行姿态的解算-Data the aircraft gyroscope given, respectively, through the list like, like Gemini, four sub-sample method Attitude solver
L3G4200D
- 陀螺仪的具体工作过程，指的是在无人机行业的应用-Detailed work process of gyroscope, refers to the application of unmanned aerial vehicle (uav) industry
Attitude-Algorithm
- 两种基于互补滤波的姿态算法，对陀螺仪和加速度计进行数据融合，解算姿态。一种使用了梯度下降算法，另一种使用反馈修正和李雅普诺夫分析。-Two algorithms for attitude estimate based on complementary filtering. Data form Gyroscope and Accelerometer are fused. One is based on gradient descent algorithm while the other is ba
psd-glpu
- matlab功率谱图，可以通过它对陀螺仪或加速度进行噪声误差分析，已经取得很好效果，请放心使用-matlab power spectrum, it can be a gyroscope or an acceleration noise error analysis, we have achieved very good results, ease of use