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gyro_EKF
- 给出了一种基于陀螺和四元数的EKF卫星姿态确定算法，非常实用-is based on a gyroscope and quaternion the EKF satellite attitude determination algorithm, a very practical
EKF
- 卫星姿态确定的卡尔曼滤波，使用matlab 仿真的姿态确定-satellite attitude determination
choi_thesie_1989
- satellite attitude determination
SpacecraftAttitudeDeterminationUsiGlobalPositioni
- Spacecraft Attitude Determination Using Global Positioning Satellite Signals - Johnson-Spacecraft Attitude Determination Using Global Positioning Satellite Signals- Johnson
OMNeTbasedsatelliteposecontrolsimulation
- 针对三轴稳定卫星的姿态控制系统,在离散事件仿真平台OMNeT ++的 基础上,建立了一个以星敏感器和陀螺为敏感器,反作用飞轮为执行机构的闭环 控制仿真系统。采用双矢量定姿算法和P ID控制算法,对该卫星在对地定向模 式下的控制精度进行了仿真。仿真结果清晰地反映了星敏感器和反作用飞轮输 出延时对控制精度的影响。整个仿真系统符合面向对象和模块化的程序设计理 念,并实现了仿真程序的重用。-For the three-axis stabilized satellite attitu
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
hods
- 陀螺_星敏感器的微小卫星姿态确定方法determination methods-_ Gyro micro satellite star sensor attitude determination methods
gyro_EKF
- Aiming at determining the satellite attitude precisely，the gyros bias and m isa lignment were compensated in time by using the quaternion of star-sensor and extended Kalm an filter．The related module of the filter was derived．The theoretic accuracy o
attitude
- 北斗卫星导航测姿系统多天线空间配置设计 matlab程序 3天线-Configuration design of multi-antenna space for Beidou satellite navigation and attitude determination system
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