1) Attitude determination
定姿
1.
The paper establishes the algorithm model of the spacecraft attitude determination in detail according to the high dynamic spacecraft motion model.
本文针对Galileo系统提供的三载波信号和高动态用户的运动规律 ,详细推导了空间飞行器姿态确定的算法模型 ,提出了一种将三载波模糊度解算技术 (TCAR)应用于高动态定姿中的新方法 。
2) stable location and pose
稳定位姿
1.
The stability analysis of assembly process was implemented from the two respects of the stability of components assembled and the stable location and pose of moving subassemblies.
建立了面向装配过程稳定性分析的装配模型,从装配操作的稳定性和子装配体稳定位姿两方面分析装配过程的稳定性。
3) attitude determination
姿态确定
1.
Application of adaptive extended Kalman filter in spacecraft attitude determination system;
自适应扩展卡尔曼滤波在卫星姿态确定系统中的应用
2.
Particle filtering-based algorithm for micro-satellite attitude determination;
基于粒子滤波的微小卫星姿态确定算法
3.
Study on multiple GPS antennae and MEMS based on INS integrated attitude determination system;
多天线GPS和微机械惯导组合进行姿态确定
4) initial attitude alignment
初姿标定
5) attitude survey
姿态定向
6) integrated attitude determination
组合定姿
1.
The method of integrated attitude determination based on inertial navigation system and star sensor is researched in this paper.
研究了利用惯性导航系统与星敏感器进行组合定姿的方法。
2.
The method of integrated attitude determination based on inertial navigation system and celestial navigation system is researched in this paper,the state equation and measurement equation of integrated navigation systems were established.
研究了利用惯性导航系统与天文导航系统进行组合定姿的方法;构造了惯导/天文组合导航系统的状态方程和量测方程;采用卡尔曼滤波技术设计了惯导/天文组合定姿算法。
补充资料：美姿姿
1.同"美孜孜"。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条