搜索资源列表
UKF_GPS
- 利用UKF融合算法在融合多传感器数据加上GPS实现多数据融合，最后进行姿态解算-UKF fusion algorithm in use multi-sensor data fusion plus GPS multi-data fusion, and finally the attitude solution
zitaijiesuan
- 本人编写的动态姿态解算程序，有三子样、kalman等算法，附有mti实测数据。-I prepared a dynamic attitude solver, there are three sub-sample, kalman algorithms, with mti measured data.
MEMS-attitude-estimation
- 一篇关于AHRS动态姿态解算的好文章，英文题目A Robust Nonlinear Observer for Real-Time Attitude Estimation Using Low-Cost MEMS Inertial Sensors-An excellent article about AHRS attitude dynamic solver, the English title A Robust Nonlinear Obse
quadrotor-according-to-apm-dmp
- 这是IAR工程，用于freescale k60 mcu。PID部分借鉴了apm开源飞控，姿态解算使用了dmp，遥控器部分是解码pwm信号。工程中也有互补滤波的全套代码，只是没有使用。代码写得很乱，仅供参考。-This is the IAR works for freescale k60 mcu. PID section draws apm open source flight control, attitude solver uses
MWC
- MWC飞控代码，可实现四轴飞行器空中姿态解算和运动控制。-MWC FM
MPU6050_DMP
- 基于stm32f107的mpu6050姿态解算源码。-Based stm32f107 of mpu6050 attitude count source solution.
Attitude-arithmetic-forSTM21
- MPU6050+HMC5883+STM32平衡小车，姿态解算MCU源代码，串口发送。这个可以用IMU软件查看数据变化情况。-MPU6050+ HMC5883+ STM32 balanced car, attitude solution MCU source code and serial port. This software can be used to view the data changes IMU.
Myfly_IMU6050_ZI_250_dinggao
- 本人做的四轴飞行器，可以平稳飞行，可平稳定高飞行，内含mpu6050，5883l，气压计，超声波驱动，四元数姿态解算，串行PID控制姿态和定高。-I do four-axis aircraft, a smooth flight, can fly high level of stability, containing mpu6050,5883l, barometer, ultrasound drive, quaternion attitu
Myfly_IMU6050_ZI_250_yaokong
- 本人做的四旋翼飞行器源码，这个是纯遥控版，可以实现稳定飞行，内含mpu6050,5883l，等传感器驱动，以及四元数姿态解算，和PID，以及遥控的解锁上锁等-I do four rotorcraft source, this is a pure version of the remote control, you can achieve a stable flight, containing mpu6050,5883l, and oth
MPU6050
- 本程序实现如下功能：开机后，先初始化MPU6050等外设，然后利用DMP库，初始化MPU6050及使能DMP，最后，在死循环里面不停读取：温度传感器、加速度传感器、陀螺仪、DMP姿态解算后的欧拉角等数据，通过串口上报给上位机（温度不上报），利用上位机软件（ANO_Tech匿名四轴上位机_V2.6.exe），可以实时显示MPU6050的传感器状态曲线，并显示3D姿态，可以通过KEY0按键开启/关闭数据上传功能。同时，在LCD模块上面显示温
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.
sysuf
- 用四元数法的捷联惯性导航姿态解算程序,主要用于飞行控制-Quaternion method of SINS Attitude solver, is mainly used for flight control
-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 test
inertial-navigation-algorithm
- 捷联惯性导航姿态解算原理及核心算法,从原理到最终程序实现-Strapdown inertial navigation attitude algorithm principle and the core algorithm, the principle to the final program
08.-MPU6050
- 四元数姿态解算的程序，自己本科时候的毕业设计就是这个。-attitude caculate
plane
- 四旋翼控制程序 姿态解算 pid控制 无线数据传输-Quadrotor attitude control program solver pid control wireless data transmission
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
imu_kF
- 用了arduino ATMEGA328 作为MCU，IMU用了MPU6050,源码内容主要进行了IMU的姿态解算，适合四轴飞行器初学者-With the arduino ATMEGA328 as MCU, the company used MPU6050, main source content of IMU attitude algorithm, suitable for four axis aircraft beginners
kalmanfilter
- 飞行器姿态解算中用到的卡尔曼滤波的simulink模型-simulink model of kalman in AHRS
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