strarpdown attitude algorithm 捷联姿态算法
SINS attitude algorithm 捷联惯导系统姿态算法
updating attitude algorithm 姿态更新算法
attitude algorithm for SINS 捷联姿态解算
attitude updating algorithm 姿态更新算法
Attitude updated algorithm 姿态更新算
The high efficiency N fast SINS attitude algorithm is continued , and after comparing and analyzing existing SINS attitude algorithms ,we drew a conclusion that four-order runge-kutta is more suited in application.
继续研究高效快速的捷联姿态算法，对现有的捷联姿态算法进行了比较和分析，得出了四阶龙格库塔法更适合实际应用的结论。
参考来源 - 捷联惯性系统关键技术研究All applied methods are directly used the angular rate measurements of gyroscopes. Therefore, there is small error rather than the rotation angle calculation based attitude algorithm.
上面所采用的方法可以直接利用陀螺仪测量的旋转速率,该算法误差比基于旋转角计算的姿态算法误差要小。
参考来源 - 捷联惯性导航系统的姿态算法研究·2,447,543篇论文数据，部分数据来源于NoteExpress
The circuit and software of attitude algorithm is designed.
设计了姿态解算模块的硬件电路和软件实现程序。
Sensor errors are the main factors which have influence on attitude algorithm accuracy.
传感器误差是影响姿态解算精度的主要因素。
The random constant drift of the low accuracy gyroscope has a serious effect for attitude algorithm.
弹载低精度陀螺仪的随机常值漂移严重影响到弹体姿态解算的精度。
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