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AttDet_23_Oct_2008
- 利用gps多天线载波相位技术，确定姿态软件。-The use of multi-antenna gps carrier phase technology, attitude determination software.
directattitudeError
- 采用直接法进行姿态参数的求解仿真，对姿态求解有很大的帮助-Posture parameters using direct method for solving simulation of the gesture of great help to solve
EKF_MEMS
- 姿态信息是飞行控制中最关键的参数之一,因此姿态测量成为飞行控制系统首要解决的问题。利用多MEMS传感器研制了一种微型姿态测量系统。利用三轴MEMS加速度计和三轴MEMS陀螺数据,由方向余弦矩阵的姿态表示形式推导了扩展Kalman滤波方程,解算出飞行器的俯仰角和横滚角 设计专家系统判断飞行器的运动状态,并根据该状态调整滤波算法中的测量噪声矩阵,使系统可同时满足静态情况和动态情况的使用 利用空速和高度数据对俯仰角进行修正,利用GPS解算航向角。将实验结果与国外最新 的商用自动驾驶仪的姿态结果进行
ADU5600-5630
- ADU5600/5630姿态方位组合导航系统用户手册-ADU5600/5630 posture position navigation system user manual
LAMBDA
- GPS载波相位测量中LAMBDA算法整周模糊度求解程序；是GPS姿态动态测量入门级算法。-ambiguity solution for gps in carrier measurement,is the basic algrithom for gps attitude measurement on the fly.
sinsgpstcm2kf
- 程序用仿真的方法编制了捷联惯导系统的姿态和航向角解算算法，适合学习算法用。-it is a good programme for them who is studying the algorithm of strapdown inertial navigation.
22
- 捷联惯性导航将惯性测量元件（陀螺仪和加速度计）直接装在飞行器、舰艇、导弹等需要诸如姿态、速度、航向等导航信息的主体上C源码-Strapdown inertial navigation inertial measurement elements (gyroscopes and accelerometers) directly installed in aircraft, ships, missiles and other needs such as attitude, speed, heading
SINS-MatlabImplement
- 导航坐标系：东-北-天 载体坐标系：右-前-上 姿态角范围：-PI/2<=pitch<=PI/2, -PI<roll<=PI, -PI<yaw<=PI 注意程序中方位北偏西为正(Navigation coordinate system: East North day Carrier coordinate system: right - front - up)