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191208pttj9oofqzoj63go
- 四元数算法微四轴姿态解算源码。拿出来和大家一起分享。-Quaternion algorithm source micro-axis attitude solution. Out and share with everyone.
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,
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
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
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.
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
RagingFire_Fly
- 这是一款开源飞控,小四轴的源代码,代码精简,适合初学者学习,但是里面的姿态解算算法输出不够理想。-This is an open source flight control, a small four-axis source code, streamlined code, suitable for beginners to learn, but inside the pose algorithm algorithm output is not ideal.
7.Kalman_AHRS
- 基于kalman的姿态解算算法 AHRS称为航姿参考系统包括多个轴向传感器,能够为飞行器提供航向,横滚和侧翻信息,这类系统用来为飞行器提供准确可靠的姿态与航行信息。-kalman AHRS
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
FreeIMU
- 6轴或者9轴(加速度计、陀螺仪、磁位计)姿态解算算法(6 axis or 9 axis attitude calculation algorithm)
经典的Carmack求平方根算法
- 经典的Carmack求平方根算法,, 采集九轴传感器数据, 解算姿态(Classic Carmack square root algorithm)
二轮自平衡小车
- 自平衡小车、MPU6050、姿态解算的算法C语言实现(Self balancing vehicle based on STM32)
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)
MPU6050姿态解算STM32源码
- stm32码源实现mpu6050的三种姿态解算算法(Three algorithms of attitude calculation for mpu6050 based on STM32 code source)
姿态解算
- PX4上修改来的姿态结算算法,根据九轴传感器计算欧拉角(The modified attitude settlement algorithm on PX4 is used to calculate the Euler angle based on the nine axis sensor)
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)
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
六轴姿态解算
- MPU6050传感器的六轴姿态解算算法代码(Six-Axis Attitude Solution Algorithmic Code for MPU6050 Sensor)
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
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)