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- 利用kalman算法计算运动物体的姿态角-Algorithm using kalman attitude angles of moving objects
MultiWii_dev_20111017
- MultiWii飞控程序，包括飞行姿态、输入输出处理等控制。-MultiWii flight control procedures, including control of the flight attitude, the input and output processing.
ars
- 用于四轴飞行器的姿态算法，内含各种矩阵加减乘转置、求逆等运算，及姿态kalman滤波算法，可适用于低速旋翼机的姿态导航-For four-axis spacecraft attitude algorithm, containing a variety of matrix addition and subtraction to multiply the transpose and inverse operations, and attitude Kalman filtering algorithm
kaermanlvbo
- 惯性器件姿态解算,用于姿态解算，才有用卡尔曼滤波和数据融合的方法-Inertial attitude solution
MPU6050_stm32
- stm32读取MPU6050加速度、角速度和姿态角-stm32 read MPU6050 acceleration, angular velocity and attitude angle
DMPaccgroy
- 功能mpu6050内部自带DMP实现姿态解算算法，采用的单片机是msp430，-DMP achieve functional mpu6050 own internal attitude solver algorithm, using the microcontroller is msp430,
MPU6000
- Cortex M3 LPC1768单片机 通过IIC与SPI通信交叉读取MPU6000 三轴陀螺仪传感器的加速度 角速度。可用于运动物体姿态检测与倾角测量，可给产品带来较强的用户体验！-Cortex M3 LPC1768 microcontroller via SPI IIC communication with cross-axis gyro sensor reading MPU6000 acceleration angular velocity. Can be used for motion
Fly-4
- 四旋翼源码 GY86姿态解算+PID控制 -Aircraft source GY86 attitude solution+PID control
3D-display
- 这个软件用来显示IMU解算出的姿态。通过串口接收IMU的姿态数据，显示在上位机上，为IMU的姿态解算验证提供便利。-This software functions as a display of the attitude of a IMU. It takes the data sent by the IMU, and display the attitude of the IMU in 3D form on the PC, which easies the developement of att
msp430
- 1.机架是上一届准备国赛前买的，电机是空心杯（2000转/min） ，电池是11.1V的航模电池 2.采用2块msp430f149最小系统做飞控板，一块用来姿态控制，一块用来完成题目要求，两者之间通过串口通信 3.陀螺仪用的是MPU9150（九轴），自带有地磁传感器，不需要再加地磁传感器 4.数据融合是靠MPU9150的内部DMP处理输出（该部分程序时移植32单片机的，针对430的时钟频率对该部分程序做了一些调整） 5.姿态控制算法是PID-1 rack is the last
TWO-MOTOR-MPU6050
- 应用于两轴飞行器的测试，能测试多轴或者两轴飞行器DIY的两轴平衡控制，空间姿态解算-Used in aircraft testing two axes, to test the multi-axis or two-axis aircraft DIY balance control two axes, spatial attitude solution
fly
- 自己做的四轴飞行器源码，用的是9150做姿态检测和M4做主控。相当值得啊-Do their own quadrocopter source, using a 9150 do attitude detection and M4 do master. Well worth ah
AHRS
- 基于加速度、角速度的快速六轴姿态解算 -Based on acceleration, angular velocity of fast six-axis attitude algorithm based on acceleration, angular velocity of the fast six-axis attitude solution
AHRS
- 基于加速度、角速度的快速九轴姿态解算,选用传感器为MPU6050+HMC-Based on acceleration, angular velocity quick nine-axis attitude solution, the choice of sensor MPU6050+HMC
keikong_V1.1
- 基于stm32的四轴飞行器源码，使用mpu6050模块,四通PWM捕获，PID,姿态解算-Four axis based on stm32 aircraft source, the use of mpu6050 module, four-way PWM capture, PID, the attitude algorithm
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
MPU-9150-GY-9150-
- MPU-9150 GY-9150 九轴姿态资料和测试代码,详细-MPU-9150 GY-9150 9-axis attitude information and test code, detailed
AHRS-DATA
- 基于惯性传感器的姿态解算，输出四元数和欧拉角，常用于惯性导航。-Based on the attitude of the inertial sensor, the output of four elements and Euler angles, commonly used in inertial navigation.
crazepony-firmware-none-master
- 微小型四轴开源飞控程序，采用互补滤波算法求得姿态，并做双级P控制！ID-A miniature four axis flight control source program, using complementary filter algorithm to obtain the attitude, and double PID control!