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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
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
attitude-determination-with-GPS-
- 多天线姿态确定工具箱，包括星历读取、单点定位、差分定位、坐标转换、定姿等-In this paper a MATLAB toolbox for determining the attitude of a rigid platform by means of multiple non-dedicated antennas using global positioning system is presented. The programs embedded in this toolbox cover
StarGuide
- 通过与导航星库中的参考星进行三角形匹配实现姿态确定-satellite attitude determination