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给出了一种基于陀螺和四元数的EKF卫星姿态确定算法,非常实用-is based on a gyroscope and quaternion the EKF satellite attitude determination algorithm, a very practical
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利用matlab数值计算的强大功能和,建模容易实现的特点"进行了捷联式惯性导航系统的仿真研究,对四元数及姿态矩阵等的解算采用编程实现"陀螺仪和加速计的建模用.-Matlab numerical calculation using the power and, modeling the characteristics of easy to implement " a strapdown inertial navigation system of the simulation study a
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The modeling and attitude stabilization control problems of a four-rotor vertical takeoff and landing unmanned air vehicle (UAV)
known as the quadrotor are investigated.The quadrotor’s attitude is represented by the unit quaternion rather than Eule
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对加速度,陀螺仪(IMU)数据,进行四元数更新,解算姿态角,与实际转角的对比分析-For acceleration gyroscope (IMU) data, carries on the quaternion update, calculating attitude Angle, and the actual Angle of comparison and analysis
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采用梯度下降法,更新加速度和陀螺仪数据的四元数,解算姿态角-Using the gradient descent method, update acceleration and quaternion gyroscope data, calculating attitude Angle
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使用STM32F103读取MPU6050六轴陀螺仪数据采用dmp库函数计算姿态角,四元数,控制风力摆的风机转速,2015全国电子设计大赛题目。-STM32F103 read MPU6050 use a six-axis gyroscope data calculated using the dmp library functions attitude angle, quaternion, put the fan speed control of the wind, the National El
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基于飞思卡尔半导体公司的K60单片机的加速度陀螺仪采集程序,本程序是用MPU6050传感器的DMP库实现四元数的输出。-K60 MCU based on freescale semiconductor acceleration gyroscope collection procedures, this procedure is to use the DMP MPU6050 sensor library realize the output of the quaternion.
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所有数据融合(包括dmp输出数据,如加速度计数据,
陀螺仪,6轴四元数和内部磁力计数据)通过7态13测量
EKF(扩展卡尔曼滤波器)/无限卡尔曼滤波器(UKF)/ Cubature卡尔曼滤波器(CKF)算法/
平方根均方卡尔曼滤波器(SRCKF)算法。-All data fusion (including the data of dmp output, such as the accelerometer data,
gyroscope, 6-axis quaternion
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陀螺仪原始数据处理,通过四元数计算姿态角(Gyroscope raw data processing, through the quaternion to calculate the attitude angle)
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四元数姿态解算互补滤波无人机IMU
可用于要求精度不高于0.5的无人机使用(The updating attitude algorithm using gyroscope was studied both in theory and execution of computer operation, and then, the quaternion theory based on Runge-Kutta method was choose.)
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