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Baxis_gyroscope__IDG300_source
- 二轴陀螺仪IDG300源程序，主要实现姿态实现算法和温度补偿及校准,B-axis gyroscope IDG300 source, the main algorithm realize realize posture and temperature compensation and calibration
ADC_4PWM_3_Done
- DSP TMS320F2812的四轴飞行器控制程序，包含四路PWM输出，AD采集，及陀螺仪和加速度计的数据融合代码，姿态调整采样简单的PID控制算法-DSP TMS320F2812 four shaft vehicle control program, including four road PWM output, AD collection, and gyroscope and accelerometer data fusion code, attitude adjustment sampli
Kalman
- 卡尔曼算法结合陀螺仪和加速计的滤波算法！-Kalman filtering algorithm combined with gyroscopes and accelerometers algorithm!
main
- 三轴陀螺仪测角度，加速度，用于自由摆，控制摆的平衡，运用PID算法平稳控制-Three-axis gyroscope measurement angle, acceleration, for free-swing, swing the balance of control, the use of smooth control PID algorithm
kalman
- 卡尔曼滤波算法，输入陀螺仪测得的角速度、加速度计测得的角度，输出量为滤波之后的角度，消除零漂。-Kalman filtering algorithm, the input gyroscope angular velocity and acceleration of the measured meter measured Angle, Angle after output for filtering, to eliminate the zero drift.
MPU6050_F149
- 陀螺仪例程，主要针对MPU6050三轴传感器设计控制算法。-Gyro routines, mainly for MPU6050 triaxial sensor design control algorithms.
My-understanding-of-control
- 飞机姿态算法。从这篇文章是我尝试的飞行器姿态检测采用四元数方法,然后利用卡尔曼滤波算法,并尝试卡尔曼滤波器耦合的多个状态变量可以是一个复杂的过程,线性系统状态估计进行了简单的解耦,将最优估计的态度和最优估计陀螺漂移,通过这种方式,可以通过直观的方法来调整参数的两个部分。-Aircraft attitude algorithm.From this article is my attempt to spacecraft attitude detection by using the quaterni
msp430
- 1.机架是上一届准备国赛前买的，电机是空心杯（2000转/min） ，电池是11.1V的航模电池 2.采用2块msp430f149最小系统做飞控板，一块用来姿态控制，一块用来完成题目要求，两者之间通过串口通信 3.陀螺仪用的是MPU9150（九轴），自带有地磁传感器，不需要再加地磁传感器 4.数据融合是靠MPU9150的内部DMP处理输出（该部分程序时移植32单片机的，针对430的时钟频率对该部分程序做了一些调整） 5.姿态控制算法是PID-1 rack is the last
gyroaacc
- 这是加速计和陀螺仪融合提取算法，并通过电灯控制来表示是否读取合理结果-This is a fusion of accelerometers and gyroscopes extraction algorithms, and to indicate whether a reasonable result read by lamp control
pinghengchestc
- 平衡车，小车直立，算法控制，PID，陀螺仪姿态角控制-The balance of the car, the car upright, control algorithm, PID, the gyro attitude angle control
KK_C
- 四轴飞行器控制程序，包含四路PWM输出，AD采集，及陀螺仪和加速度计的数据融合代码，姿态调整采样简单的PID控制算法-Quadrocopter control procedures, including four PWM outputs, AD acquisition, and gyroscope and accelerometer data fusion code, attitude adjustment sampling simple PID control algorithm
siyuansu-ahrs
- AHRS,导航算法，四元素算法，姿态结算功能，陀螺仪，加速度计-AHRS, navigation algorithm, four-element algorithm, attitude clearing functions, gyroscopes, accelerometers
mpu-kalman
- 用于kalman的计算，导航算法滤波功能，陀螺仪加速度计的滤波，mpu6050-For kalman calculations, navigation algorithm filtering, gyroscope accelerometer filtering, mpu6050
MPLv3.3.0
- Invens e 陀螺仪驱动以及sensor fusion算法，Android系统-Invensense gyro driver and sensor fusion algorithm for Android
adc
- 使用stc公司的IAP15W系列单片机作为主控制器，使用mpu6050的陀螺仪，加速度计，二阶微分滤波，速度反馈，PID的速度控制算法。宏晶杯大赛作品-Use stc s IAP15W series microcontroller as the main controller, use mpu6050 gyroscopes, accelerometers, second-order differential filtering, speed feedback, PID speed control
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
windPendulum8_16_04_36
- 2015年全国大学生电子设计竞赛B题——风力摆控制系统，全国一等奖源代码，使用MPU6050陀螺仪，分段PID算法完成。-2015 undergraduate national electronic design contest subject B——wind pendulum control system，got first place，based on MPU6050 and PID segmentation algorithm.
stm32f4_mpu9250-master
- 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
BMI160
- 陀螺仪 加速度 角度 C语言 IMU算法实现 亲试可用-borch bmi 160 driver, c(View point C of IMU algorithm implementation pro acceleration gyroscope is available - 160 driver borch bmi, C)
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)