Description: 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 Platform: |
Size: 237225 |
Author:李然 |
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Description: 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 Platform: |
Size: 236544 |
Author:李然 |
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Description: 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 and the attitude quaternion matrix solvers such as the use of programming" gyroscope and accelerometer Modeling used. Platform: |
Size: 104448 |
Author:宋磊 |
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Description: 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 Euler angles to
avoid singularity problem. Taking dynamical behavior of motors into consideration and ignoring aerodynamic effect, a nonlinear
controller is developed to stabilize the attitude.The control design is accomplished by using backstepping control technique.The
proposed control law is based on the compensation for the Coriolis and gyroscope torques. Applying Lyapunov stability analysis
proves that the closed-loop attitude system is asymptotic stable. Moreover, the controller can guarantee that all the states of the
system are uniformly ultimately bounded in the presence of external disturbance torque.The effectiveness of the proposed control
approach is analytically authenticated and also validated via simulation study. Platform: |
Size: 53248 |
Author:balaji |
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Description: 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 Platform: |
Size: 1024 |
Author:志祥 |
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Description: 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 Electronic Design Contest 2015 title. Platform: |
Size: 13858816 |
Author:龙泰 |
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Description: 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. Platform: |
Size: 2422784 |
Author:xiaoxiong |
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Description: 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) Platform: |
Size: 1024 |
Author:tome
|
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Description: 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.) Platform: |
Size: 3072 |
Author:xiixuu |
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Search - quaternion gyroscope