搜索资源列表
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
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姿态解算
- STM32对MPU6050的四元数姿态解算，
-Settler-V3
- 自己写的一个使用STM32的小四轴代码，包含了MPU6050的使用，飞行的姿态解算，PWM的控制和串级PID控制，经过测试可使用-Write your own STM32 using a small four-axis code, including the use of MPU6050 flight attitude algorithm, PWM control and cascade PID control, can be tested using
attitude-solution
- 基于stm32的mpu6050姿态解算，yaw角数据没有进行处理，可以开发平衡车或进一步融合九轴数据完善yaw角数据进行四轴开发-Based on the mpu6050 STM32 attitude solution, yaw angle data is not processed, you can develop a balanced car or further integration of the nine axis data to improve the yaw angle data
4zhouV01
- 基于stm32的四轴无人机的姿态解算与控制系统设计-Attitude calculation and control system design of four axis unmanned aerial vehicle based on stm32
Kalman_AHRS
- 基于STM32和MPU6050的姿态解算-Based on the STM32 and MPU6050 attitude algorithm
STM32--mpu6050
- 完成mpu6050的姿态角解算，包括卡尔曼，一阶以及二阶滤波算法-caculate the angels of the mpu6050
STM32_AHRS_WorkDir
- 一套注释详细的飞控源码。飞控芯片采用了stm32，包含pid 姿态解算 数据融合等。-A set of detailed notes of the flight control source. Flight control chip uses stm32, pid attitude solution comprising data fusion.
四旋翼源代码
- 基于STM32F4的四轴航拍平台。以STM32F407为控制核心，四轴飞行器为载体，辅以云台的航拍系统。硬件上由飞控电路，电源管理，通信模块，动力系统，机架，云台伺服系统组成。算法上采用简洁稳定的四元数加互补滤波作为姿态解算算法，PID作为控制器，实现飞行，云台增稳等功能(Four axis aerial platform based on STM32F4. Taking STM32F407 as the control core, the four axis flying vehicle as
MPU6050姿态解算STM32源码（DMP）
- STM32解算MPU6050工程文件，IIC读取6050数据，带DMP 。(STM32 calculation of MPU6050 engineering documents)
二轮自平衡小车
- 自平衡小车、MPU6050、姿态解算的算法C语言实现(Self balancing vehicle based on STM32)
MPU6050姿态解算STM32源码
- stm32码源实现mpu6050的三种姿态解算算法(Three algorithms of attitude calculation for mpu6050 based on STM32 code source)
MPU-6050模块资料
- 3轴陀螺仪、3轴加速器 姿态解算核心算法(a 3-axis gyroscope and a 3-axis accelerometer)
实验32 MPU6050六轴传感器实验
- 使用STM32F4来驱动MPU6050，读取其原始数据，并利用其自带的DMP实现姿态解算，结合匿名四轴上位机软件和LCD显示(Using STM32F4 to drive MPU6050, read its original data, and use its own DMP to realize attitude calculation, combined with anonymous four axis PC software and LCD display)
四轴测试
- IMU数据应用于UAI四轴无人机，实现油门控制，pid调速，姿态解算等功能(The IMU data is applied to the UAI four axis UAV to realize throttle control, PID speed regulation, attitude calculation and other functions.)
四元数AHRS姿态解算和IMU姿态解算分析
- 四元数AHRS姿态解算和IMU姿态解算分析(Four element number AHRS attitude calculation and IMU attitude calculation analysis)
STM32F407_FCVGTx_ANO 飞控
- stm32飞控源代码内置pid算法陀螺仪姿态解算模糊pid等(STM32 Flight Control Source Code Built-in Pid Algorithms Gyroscope Attitude Resolution Fuzzy Pid and so on)
MPU6050姿态解算STM32源码（DMP）
- 通过stm32 采集并通过DMP解算 MPU6050的角度，，通信采用IIC通信(The angle of the MPU6050 is solved by stm32 and calculated by DMP. The communication uses IIC communication.)
imu - 2020.09.18
- 基于stm32f103c8t6的姿态解算源码，icm和imu系列均可稳定使用(Based on stm32f103c8t6 attitude calculation source code, ICM and IMU series can be used stably)