搜索资源列表
CF_2
- 两自由度互补滤波的Matlab仿真程序,数据源和测试数据均为Pixhaw飞控采集(Matlab simulation program of two degree of freedom complementary filter, data source and test data are Pixhaw flight control acquisition)
motion_driver-5.1.2
- InvenSense陀螺仪姿态解算,直接输出四元数,省去姿态融合算法的编写,适用于飞控(The attitude calculation of InvenSense gyroscope outputs four elements directly, and avoids the compilation of attitude fusion algorithm, which is suitable for flight control)
36692817DXsinscal_JZ
- 自己仿真的四元数法的龙格库塔的姿态解算matlab仿真(Their simulation of the quaternion method of runge kutta the attitude algorithm of matlab simulation)
飞行器固件
- 姿态解算融合,是Crazepony和核心算法 使用的是Mahony互补滤波算法,没有使用Kalman滤波算法(The fusion of attitude calculation is Crazepony and the core algorithm The Mahony complementary filtering algorithm is used, and the Kalman filtering algorithm is not used)
CF_v1
- 加计陀螺互补滤波,姿态解算,非常好用,简单实用,希望帮助到大家。(It is very useful, simple and practical. It is hoped to help you.)
STM32F103C8T6-IMU-6050
- stm32f103硬件IIC读取MOU6050驱动代码,带DMP程序(STM32F103 hardware IIC reads the MOU6050 driver code, with the DMP program)
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)
imu
- 四元数姿态解算互补滤波无人机IMU 可用于要求精度不高于0.5的无人机使用(The updating attitude algorithm using gyroscope was studied both in theory and execution of computer operation, and then, the quaternion theory based on Runge-Kutta method was choose.)
ANO-MR-F1
- 四轴PID控制,MPU6050的姿态解算,STM32F103的串级PID。(Four axis PID control, MPU6050 attitude calculation, STM32F103 cascade PID.)
MPU6050 亲测可用
- keil MPU 实现姿态解算算法的源代码,亲测可用~~~~(keil MPU pose_estimation)
MPU6050六轴传感器实验
- 实验器材: 探索者STM32F4开发板 实验目的: 学习MPU6050 六轴传感器(三轴加速度+三轴陀螺仪)的使用. 硬件资源: 1,DS0(连接在PF9) 2,串口1(波特率:115200,PA9/PA10连接在板载USB转串口芯片CH340上面) 3,ALIENTEK 2.8/3.5/4.3/7寸TFTLCD模块(通过FSMC驱动,FSMC_NE4接LCD片选/A6接RS) 4,KEY0按键(连接在PE4) 5,MPU6050传感器(连接在PB8(
MK60FX15开源
- 实现MPU6050的姿态解算,K60的程序(Realizing the attitude calculation of MPU6050, K60 program)
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.)
windows
- 计算角速度、加速度、磁场、GPS数据。姿态解算器,配合动态卡尔曼滤波算法,能够在动态环境下准确输出 模块的当前姿态,姿态测量精度静态0.05 度,动态0.1 度,稳定性极高,性能甚至优 于某些专业的倾角仪!(Calculation of angular velocity, acceleration, magnetic field, GPS data)
基于STM32F4的四轴航拍飞行器
- 本设计是基于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。具有灵活轻盈,延展性,适应性强好等特点。(This design is based on STM32F4's four axis aerial platform. Taking STM32F407 as the con
NamelessCotrunQuad_V1.7.5.1
- 参考国内外主流 飞控(APM、 Pixhawk、 Autoquad、 MWC、 CC3D、 INF、 ANO、 LIGHT 等) 的算法与整体 框架的进行深入学习基础上, 经过软、 硬件的精心设计, 继承与发展, 目前飞控整体功 能相对完善, 主要功能有: 姿态自稳、 超声波、 气压计定高, 低空光流定点悬停、 户外 GPS 定点, GPS 模式下定速巡航、 一键返航着陆等功能, 涵盖飞控学习主要核心算法: 传感器滤波(一阶 RC、 二阶巴特沃斯、 带阻滤波、 陷波滤波等) 、 姿态解
QEKF1
- 加速度计、陀螺仪、磁力计的扩展卡尔曼滤波融合程序,里面附有数据,可直接运行。(Accelerometer, gyroscope, magnetometer extended kalman filter fusion program, with data, can be directly run.)
MPU6050姿态解算STM32源码(卡尔曼滤波)
- MPU6050是我们常用的六轴空间位置处理芯片,次文档使用卡尔曼滤波的方式使数据更加的准确(MPU6050 is our commonly used six-axis spatial position processing chip. Kalman filter is used in sub-documents to make the data more accurate.)
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)