搜索资源列表
kalman
- 采用STM32硬件I2C，DMA方式读取总线数据进行kalman滤波解算姿态位置。-Using STM32 hardware I2C, DMA mode data read bus kalman filter solver attitude position.
sins
- 惯导仿真部分模块化，标准化，分为IMU模块，初始对准模块，SINS解算模块，SINS性能评价模块，SINS解算的输出为地理坐标系内速度、经纬高、姿态角,运行INS_perforEva.m可以得到惯导仿真结果。-INS simulation part modular, standardized, divided IMU module, the initial alignment module, SINS solver module, SINS performance uation module,
atti001
- 利用四元素的方法解算卫星姿态误差估计matlab程序代码-Satellite attitude error estimate
attitutionerror1
- 利用四元素的方法解算卫星姿态误差估计的matlab程序源码- The use of four elements method solver satellite attitude error estimation matlab Open Source
quadrotor-simm
- 自己做的基于非线性动力学模型的四旋翼飞行器用的PID控制的姿态控制仿真模型和位置回路的仿真模型，inversion1是给定位置解算姿态的文件-Based on their own four-rotor aircraft nonlinear dynamic model with attitude control PID control simulation model simulation model and the position loop, inversion1 a given locati
DOF6_1
- 进行导弹六自由度弹道仿真的simulink文件，可进行弹道位置信息和姿态信息的解算-trajectory simulink
MPU9150
- mpu9150加速度，角速度，磁场，九轴传感器，基于stm32实现，采用内置bmp解算姿态角，做四轴必备。-mpu9150 acceleration, angular velocity, magnetic field, 9-axis sensor, based on stm32 achieved using the built-in solver bmp attitude angle, make the necessary axis.
MahonyUpdate
- 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
MadgwickUpdate
- 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
orientation-estimation
- 利用加速度计、陀螺仪、地磁解算姿态的好文章，英文名Design of orientation estimation system by inertial and magnetic sensors-The use of an accelerometer, a gyroscope, a geomagnetic solver attitude of good articles, the English name Design of orientation estimation system by in
jiesuandaquan
- 捷联惯导姿态位置速度高度全解算，其中程序的使用还应该按需选择和衔接-SINS Attitude Full height position and speed solver, In which the program should also demand choices and Cohesion .
MPU6500-DMP-IMU
- 该文件，包括了MPU6500的DMP库解算姿态，以及使用IMUupdate解算姿态，移植时只需修改I2C文件即可。-The file, including MPU6500 DMP library calculating posture, and using IMUupdate calculating attitude, only need to modify the I2C files when transplanting.
tuoluoyi
- 基于stm32 103系列单片机的模块集成高精度的陀螺仪、加速度计、地磁场传感器程序，采用先进的动力学解算与卡尔曼动态滤波算法，能够快速求解出模块当前的实时运动姿态。-stm32 103 series single chip microcomputer module integrated high precision gyroscope and accelerometer, the magnetic field sensor application, USES the advanced dyn
ins_jiesuan_matlab
- 本程序为捷联惯导的解算程序(由惯性器件的输出解算出飞行器的位置、速度、姿态信息-The program for the sins of the solver (by the output device calculates the inertial solution aircraft position, velocity, attitude information
minicraft
- 自己写的四轴飞行器控制程序，包括姿态检测，四元数解算，电机控制，遥控-code for four rotor
Rongekutta
- 龙格库塔算法，用于姿态角的解算，此程序采用四阶龙格库塔法进行计算。-Ronge Kutta algorithm for attitude angle calculation, this procedure using four order Ronge Kutta method.
kaemanshiyan
- 该程序为姿态卡尔曼滤波算法，可以解算出物体姿态-The program for the attitude Kalman filter can be calculated by body posture
imu_calibratio
- 通过9位置法进行加速度标定，采集旋转数据进行陀螺仪标定以及磁力计的标定，以达到减小误差为后续姿态跟踪或解算提高精度-IMU calibration
duoziyang
- 由飞机陀螺仪所给出的数据，分别通过单子样，双子样，四子样方法进行飞行姿态的解算-Data the aircraft gyroscope given, respectively, through the list like, like Gemini, four sub-sample method Attitude solver
Attitude-Algorithm
- 两种基于互补滤波的姿态算法，对陀螺仪和加速度计进行数据融合，解算姿态。一种使用了梯度下降算法，另一种使用反馈修正和李雅普诺夫分析。-Two algorithms for attitude estimate based on complementary filtering. Data form Gyroscope and Accelerometer are fused. One is based on gradient descent algorithm while the other is ba