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SOFT_DESIGN
- 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。-The design is based on a four-axis STM32F4 aerial platform. In STM32F407 as the control
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.
hubulvbo
- 基于四元数互补滤波的四轴飞行器姿态解算算法。包括四元数、互补滤波、姿态结算-Solver algorithm based on quaternion complementary filter axis spacecraft attitude. Including quaternion complementary filter, posture settlement
F4-FLYC
- 基于STM32F4的飞控程序，四元数互补滤波-Based on STM32F4 flight control procedures, quaternion complementary filter
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
- MPU6050经过互补滤波和四元数转换为欧拉角 得到稳定的三轴角度(MPU6050 is converted to Euler angles by complementary filtering and four element number to obtain a stable three axis angle)
四轴-四元数 互补滤波 串级PID测试版
- 四轴-四元数 互补滤波 串级PID测试版(Four axis - four - number complementary filter series PID test edition)
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.)
siyuanshu
- simulink模块，基于互补滤波，解四元数微分方程，更新四元数和欧拉角，更新姿态(Complementary filtering completed with attitude updating)
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