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satellite1
- 针对卫星姿态控制中的一些常见运算的源码。如，四元素与欧拉角的互换，矩阵之间的运算等-against satellite attitude control of the operation some common source. For example, four elements and Euler angle swap between the matrix, etc.
weizijisuan
- 根据GPS回传的数据，进行坐标变换，计算应该达到的姿态-Return GPS data, coordinate transformation, the calculation should reach posture
clear
- 该原代码包括捷联惯导姿态程序,位置程序以及初始对准程序,实用性强,便于学习.
Mti
- 惯性测量组件Mti进行数据采集，利用陀螺和加速度计数据进行捷联姿态角解算，采用四元数更新算法，解算周期可调。
velocitymatchsimulation
- 惯性导航的传递对准程序，一种速度加姿态的对准。
扩展卡尔曼滤波姿态解算-姿态融合
- 扩展卡尔曼滤波姿态解算，matlab程序，解算方法
C_newtyle
- 航天工程用轨道卡尔曼滤波器，姿态确定传感器组合为轨道罗盘+磁强计，是当前组合中最为常见的，适合于小型卫星-Kalman filter with orbital spaceflight, the orbital attitude determination sensor combination compass+ magnetometers, is currently the most common combination is suitable for small satellites
trajection
- 用Matlab编写的轨迹发生器，输入初始的位置速度，姿态角，姿态变化等信息，模拟得到陀螺仪输出和加速度计的输出-Written with the Matlab path generator, enter the initial position, velocity, attitude, attitude changes and other information, the simulated gyro output and the output of the accelerometer
sins
- 该程序包括了飞行器轨迹计算、陀螺和加速度计的采样输入、以及由四元素解算出的飞行器姿态、位置、速度-The program includes the aircraft trajectory calculation, the sampling gyro and accelerometer input, and the solution calculated by the four elements of aircraft attitude, position, velocity
attref
- 在磁力计、重力加速度、机体加速度计模型基础上计算姿态角参数-In the magnetometer, gravity, body accelerometer attitude angle calculated based on the model parameters
imu_ahrs
- 基于IMU(三轴角速率、三轴加速计和三轴磁场)的方位姿态解算系统(ahrs)，基于C语言开发，VC 6.0编译器，可方便的移植到其他环境。-Based on the IMU (three-axis angular rate, three-axis accelerometer and three-axis magnetic field) to locate gesture Solution System (ahrs), based on C language development, VC 6.0
openpilot_ahrs
- openpilot自动驾驶仪的姿态参考系统（AHRS）源码-openpilot Autopilot Attitude Reference System (AHRS) source
Navigation
- 利用比力、加速度信息解算出惯性导航所需的速度、位置和姿态信息-Than the use of force, acceleration of information required for inertial navigation solution to calculate the speed, position and attitude information
PID
- 航天器姿态控制PID控制仿真程序，加入干扰值。-PID control of spacecraft attitude control simulation program, by adding the value of interference.
homeword2-06
- Matlab源码，仿真飞机姿态更新，主要是捷联惯导的姿态更新-Matlab source code, simulation of aircraft attitude update, mainly SINS attitude update
satellite_orbit
- 卫星轨道方面的知识，卫星轨道姿态动力学与控制-Knowledge of satellite orbit, the satellite attitude and orbit dynamics and control
LunarAzEl
- 月球方位角与高度预测 针对月球车提出了一种基于天文观测的自主位置姿态确定方法。建立了利用天体敏感器测量得到的天体高度和方位作为观测信息的量测方程，并利用月球车运动的三阶常加速-Azimuth and highly predictive of the moon rover for astronomical observations is proposed based on the independent position and attitude determining method. Est
C_newtyle
- 航天常用姿态确定敏感器组合，太阳敏感器+速率陀螺+轨道罗盘，具体数据含义请参考章仁为的<《卫星姿态控制》>-Spacecraft attitude determination sensors commonly used in combination, sun sensor+ rate gyro compass+ tracks, the meaning of specific data please refer to Chapter Ren' s < " Satell
AttDet
- 航天器姿态确定工具包,可利用CA码和L1载波进姿态确定 -attitude determinantion tool
main_attitude_measurement
- 基于gps载波相位整周模糊度的姿态测量系统实现的主程序- the main program of attitude measuring system based on GPS carrier phase integer ambiguity