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1)  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。
2)  SINS-velocity-DGPS integration positioning and posing
SINS-速度-DGPS组合定位定姿
3)  attitude integration
姿态组合
4)  gesturecombination
姿势组合
5)  position and attitude integration
位置、姿态组合
6)  Composite attitude measurement
组合姿态测量
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。
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