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postdoctor-research-report
- 严恭敏博士后研究工作报告——捷联惯导系统动基座初始对准及其它相关问题研究报告 内容包括：大失准角下捷联惯导系统动基座初始对准，激光陀螺整周期采样对姿态解算的影响极其修正方法。SINS内杆臂效应分析与补偿，圆锥误差补偿。-Yan Gong Min postdoctoral research report- Moving Base SINS initial alignment study and other related issues Content includes: Large Mis
adis16405
- 根据ADIS16405进行姿态解算得到航向横摇纵摇-according to the ADIS16405 attitude solution obtained yaw roll pitch
SINS-algorithm
- 运用四元数方法进行捷联惯性系统的姿态解算，并由加速度计的数据和陀螺的数据计算导航参数-The four element method for strapdown inertial navigation system of the attitude calculation, and the accelerometer and gyroscope data data computation of navigation parameters
INS5
- 惯导姿态解算，根据加速度计和陀螺的测量数值，求解惯导系统的姿态，速度和位置的代码-INS attitude solution
siyuanshu
- matlab实现的四元素算法，姿态解算算法中最经典的算法-Four elements algorithm matlab implementation, attitude solution algorithm is the most classical algorithm count
matlab
- 四元数法捷联惯性导航姿态解算程序。基本的方法都有。-Matlab program for INS
Quadrotor-attitude-solution
- 本文是前人总结的，关于四轴飞行器姿态解算的，我只是加以整理，方便阅读。-This paper is a summary of the previous, about four axis aircraft attitude solution, I just tidying up, easy to read.
四旋翼微型飞行器设计
- 构建了由三轴 陀螺仪三轴加速度计和三轴磁力计组成的姿态测量系统，给出了姿态解算的具体步骤
HMC-Cor-YJ
- K60为主控芯片，MPU6050解算三维姿态角，姿态解算采用DMP和四元素算法。并带有TFT液晶触摸屏以及蓝牙4.0的开发。-Use k60 as the main control MCU。MPU6050 solving three-dimensional attitude angle, attitude solver algorithm using DMP and the four elements. And with a TFT LCD touch screen and Bluetooth
Fly_Control-1-10
- 四轴飞行器控制源代码，融合姿态解算，和电机控制，能实现悬停和数据交换。-Four aircraft control source code, the integration of gesture solver, and motor control, to achieve hover and data exchange.
IMU
- 基于LPC1114完成的MPU6050及HMC5883的IMU姿态解算代码，代码注释详细，并且已调试成功-Based on LPC1114 completed MPU6050 and HMC5883 of IMU attitude solver code, code comments in detail and have been successful commissioning
Fly-4
- 四旋翼源码 GY86姿态解算+PID控制 -Aircraft source GY86 attitude solution+PID control
mpu_6050
- MPU6050参考资料，基于飞控的姿态解算-MPU6050 reference materials, gesture-based flight control solver
fly
- MSP430F149单片机结合MPU6050传感器的姿态解算以及输出PWM的四轴飞行器源码，开发环境为IAR5.4-MSP430F149 microcontroller with MPU6050 sensor attitude solution and the PWM output of the four axis aircraft source code, development environment for IAR5.4
3D-display
- 这个软件用来显示IMU解算出的姿态。通过串口接收IMU的姿态数据，显示在上位机上，为IMU的姿态解算验证提供便利。-This software functions as a display of the attitude of a IMU. It takes the data sent by the IMU, and display the attitude of the IMU in 3D form on the PC, which easies the developement of att
Strapdown
- 捷联惯性导航算法完整版（单子样姿态解算算法）-Strapdown inertial system
APM_flight-control
- APM飞控的算法介绍，说了姿态解算，PID等，比较能从整体上理解-APM flight control algorithm is introduced that the attitude algorithm, PID, etc., more overall understanding
TWO-MOTOR-MPU6050
- 应用于两轴飞行器的测试，能测试多轴或者两轴飞行器DIY的两轴平衡控制，空间姿态解算-Used in aircraft testing two axes, to test the multi-axis or two-axis aircraft DIY balance control two axes, spatial attitude solution
apm
- APM四轴飞控的源码，姿态解算和姿态控制算法做得十分完善。-APM axis flight control source, attitude and attitude control algorithm solver has been very perfect.
dual-quanternion
- 应用对偶四元素进行组合导航解算，包括姿态解算，速度解算，位置解算-the caculation of strapdown-inertial navigation with dual-quaternion