搜索资源列表
Lizy_stm32_ADIS16407
- stm32 和adis16045 能进行通讯及姿态解算-stm32 and adis16045 can communicate and attitude solution
mpu6050-program
- 陀螺仪姿态解算 四元数 捷联矩阵的初始值计算初始四元数值 用毕卡法求解四元数更新矩阵，即捷联矩阵-Gyro attitude solution
56pry
- 采集加速度计和磁强计的数据，并做姿态解算，然后将解算的三个姿态角传到串口上，采用的单片机是stc90c51rd6+-collect the data acccelerometer and meganetometer,then calculate the attitude,at last ,send the result to the com
miniAHRS_Software
- Mini IMU AHRS上位机显示姿态解算的3D结果-Mini IMU AHRS PC display 3D pose settlement result
DirectionCosin
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准方向余弦法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard method of direction cosine
RotationVector
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准旋转矢量法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard rotation vector method to s
Euler
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准欧拉法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard eulerian method to solve the
attitude_estimator_ekf
- PixHawk飞控用EKF（扩展卡尔曼滤波）方法实现姿态解算源码-PixHawk flight control with EKF (extended Kalman filter) method of solving attitude Source
attitude_estimator_q
- Pixhawk飞控基于四元数的姿态解算源码，方法简单有效-Pixhawk flight control based on quaternion attitude algorithm source code, the method is simple and effective
Untitled3
- 基于stm32的四轴飞行器，通过IIC连接MUP6050模块，姿态解算，PID控制，输入捕获-Based quadrocopter stm32 by IIC connection MUP6050 module, attitude solution, PID control, input capture
Fly
- 飞控源码，主要讲解Mpu6050的通信方式和姿态解算-Flight control source, mainly on Mpu6050 of communication and attitude solution.
ComplementFilter
- 互补滤波，应用在INS和磁罗盘融合姿态解算，详细说明-Complementary filtering, application integration attitude in solving INS and magnetic compass, a detailed descr iption
flycontrol
- 四轴飞行器飞控程序，串级PID，外环PI内环PID，四元数互补滤波，辅助三角函数姿态解算。-Four-axis aircraft flight control procedures, Cascade PID, PI outer inner PID, quaternion complementary filter, auxiliary trigonometric attitude solution.
ANO-Settler-V3
- 匿名飞控程序，姿态解算，PID调参，自动控制-ANO flight control procedures, attitude solution, PID parameter adjustment, automatic control
UKF_GPS
- 利用UKF融合算法在融合多传感器数据加上GPS实现多数据融合，最后进行姿态解算-UKF fusion algorithm in use multi-sensor data fusion plus GPS multi-data fusion, and finally the attitude solution
zitaijiesuan
- 本人编写的动态姿态解算程序，有三子样、kalman等算法，附有mti实测数据。-I prepared a dynamic attitude solver, there are three sub-sample, kalman algorithms, with mti measured data.
MEMS-attitude-estimation
- 一篇关于AHRS动态姿态解算的好文章，英文题目A Robust Nonlinear Observer for Real-Time Attitude Estimation Using Low-Cost MEMS Inertial Sensors-An excellent article about AHRS attitude dynamic solver, the English title A Robust Nonlinear Observer for Real-Time Attitude Es
quadrotor-according-to-apm-dmp
- 这是IAR工程，用于freescale k60 mcu。PID部分借鉴了apm开源飞控，姿态解算使用了dmp，遥控器部分是解码pwm信号。工程中也有互补滤波的全套代码，只是没有使用。代码写得很乱，仅供参考。-This is the IAR works for freescale k60 mcu. PID section draws apm open source flight control, attitude solver uses dmp, remote control part is de
MWC
- MWC飞控代码，可实现四轴飞行器空中姿态解算和运动控制。-MWC FM
MPU6050_DMP
- 基于stm32f107的mpu6050姿态解算源码。-Based stm32f107 of mpu6050 attitude count source solution.