搜索资源列表
GPSData
- 上位机程序，接收STM32发送的GPS数据并按照数据存储格式进行解算，解算后的结果保存在txt文件中，供后续处理。-PC program, to receive the GPS data and transmit STM32 data storage format in accordance with solver, solver the results stored in the txt file for subsequent processing.
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
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,
pid
- 四轴PID计算代码，对四轴飞行器飞行过程中的传感器数据进行PID解算-Axis PID calculation code for Four aircraft during flight sensor data PID solver
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
PmmDecode
- 这个文件的代码用来解算PPM信号。PPM信号时用一个通道传输多路信息的一种编码方式。本代码将此此“串行”信号解码，为使用PPM信号者提供方便。-This file contains the code that decodes the PPM signal which features serial transfer of several signals in one channel. The code is dedicated to the people who needs to use P
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
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
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.
fei-control
- 飞控程序。程序结构清晰。内容丰富，姿态解算部分详细-Flight Control program. Clear program structure. Content-rich, some details,,,, Attitude Algorithm
six-axis-MPU6050_sensor
- STM32F407自带了MPU6050传感器。本章我们将使用 STM32F407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。-TheSTM32F407 have a MPU6050 sensor. I use the STM32F407 to drive the MPU6050, and read its raw data, and use its own DMP to achieve attitude calculation
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_DMP
- 基于STM32的运动姿态解算，带自动校正功能。- U57FA u4E8ESTM32 u7684 u8FD0 u52A8 u59FF u6001 u89E3 u7B97 uFF0C u5E26 u81EA u52A8 u6821 u6B63 u529F u80FD u3002
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)
CC2530 RSSI测距
- CC2530 RSSI测距，从zstack里读取RSSI的值，按模型进行解算。