搜索资源列表
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
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
Lizy_stm32_ADIS16407
- stm32 和adis16045 能进行通讯及姿态解算-stm32 and adis16045 can communicate and attitude solution
mpu6050-program
- 陀螺仪姿态解算 四元数 捷联矩阵的初始值计算初始四元数值 用毕卡法求解四元数更新矩阵，即捷联矩阵-Gyro attitude solution
56pry
- 采集加速度计和磁强计的数据，并做姿态解算，然后将解算的三个姿态角传到串口上，采用的单片机是stc90c51rd6+-collect the data acccelerometer and meganetometer,then calculate the attitude,at last ,send the result to the com
miniAHRS_Software
- Mini IMU AHRS上位机显示姿态解算的3D结果-Mini IMU AHRS PC display 3D pose settlement result
DirectionCosin
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准方向余弦法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standa
RotationVector
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准旋转矢量法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standa
Euler
- 载体的姿态解算算法是实现捷联式惯性导航系统精确导航的核心技术之一，采用了标准欧拉法求解惯性导航的位置姿态-Carrier attitude algorithm of the algorithm is to achieve strapdown inertial navigation system is one of the core technology of accurate navigation, using the standard
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
Untitled3
- 基于stm32的四轴飞行器，通过IIC连接MUP6050模块，姿态解算，PID控制，输入捕获-Based quadrocopter stm32 by IIC connection MUP6050 module, attitude solution, PID control, input capture
Fly
- 飞控源码，主要讲解Mpu6050的通信方式和姿态解算-Flight control source, mainly on Mpu6050 of communication and attitude solution.
ComplementFilter
- 互补滤波，应用在INS和磁罗盘融合姿态解算，详细说明-Complementary filtering, application integration attitude in solving INS and magnetic compass, a detailed descr iption
ANO-Settler-V3
- 匿名飞控程序，姿态解算，PID调参，自动控制-ANO flight control procedures, attitude solution, PID parameter adjustment, automatic control