搜索资源列表
HMC-Cor-YJ
- K60为主控芯片，MPU6050解算三维姿态角，姿态解算采用DMP和四元素算法。并带有TFT液晶触摸屏以及蓝牙4.0的开发。-Use k60 as the main control MCU。MPU6050 solving three-dimensional attitude angle, attitude solver algorithm using DMP and the four elements. And with a TFT LCD touch screen and Bluetooth
Fly_Control-1-10
- 四轴飞行器控制源代码，融合姿态解算，和电机控制，能实现悬停和数据交换。-Four aircraft control source code, the integration of gesture solver, and motor control, to achieve hover and data exchange.
IMU
- 基于LPC1114完成的MPU6050及HMC5883的IMU姿态解算代码，代码注释详细，并且已调试成功-Based on LPC1114 completed MPU6050 and HMC5883 of IMU attitude solver code, code comments in detail and have been successful commissioning
Fly-4
- 四旋翼源码 GY86姿态解算+PID控制 -Aircraft source GY86 attitude solution+PID control
mpu_6050
- MPU6050参考资料，基于飞控的姿态解算-MPU6050 reference materials, gesture-based flight control solver
fly
- MSP430F149单片机结合MPU6050传感器的姿态解算以及输出PWM的四轴飞行器源码，开发环境为IAR5.4-MSP430F149 microcontroller with MPU6050 sensor attitude solution and the PWM output of the four axis aircraft source code, development environment for IAR5.4
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
Strapdown
- 捷联惯性导航算法完整版（单子样姿态解算算法）-Strapdown inertial system
APM_flight-control
- APM飞控的算法介绍，说了姿态解算，PID等，比较能从整体上理解-APM flight control algorithm is introduced that the attitude algorithm, PID, etc., more overall understanding
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
apm
- APM四轴飞控的源码，姿态解算和姿态控制算法做得十分完善。-APM axis flight control source, attitude and attitude control algorithm solver has been very perfect.
dual-quanternion
- 应用对偶四元素进行组合导航解算，包括姿态解算，速度解算，位置解算-the caculation of strapdown-inertial navigation with dual-quaternion
xuanzhuan
- 利用旋转矢量算法对惯性导航数据进行解算，包括姿态解算，速度解算，位置解算。-the caculation of inertial navigation with screw algorithm
111
- 基于四元数方法的姿态解算，详细介绍了四元数解算姿态的基本方法-Quaternion method based solver, detailing the basic method solver quaternion attitude
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
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
STM32_AHRS_WorkDir
- 陀螺仪 气压计 等姿态解算，下载后可以直接运用，有配套的姿态版-Gyroscope barometer of attitude algorithm, after downloading can use directly, with forms of gesture
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
MPU9250-master
- 9轴姿态传感器MPU9250的姿态解算程序，利用了9250的磁场传感器信息，比六轴更精确-9-axis attitude sensor MPU9250 gesture solver using a magnetic field sensor information 9250, more percise than 6-axis