1) Inertial Navigation System (INS) correction
惯导系统校正
2) inertial navigation system
惯导系统
1.
Rapid matching alignment algorithm of inertial navigation system based on quaternion;
基于四元数的惯导系统快速匹配对准算法
2.
Initial alignment of laser gyroscope inertial navigation system with disturbances;
激光陀螺惯导系统扰动基础上的初始对准
3.
Performance assessment for stabilized loop of inertial navigation system based on minimum variance control
基于最小方差控制的惯导系统稳定回路性能评估
3) INS
惯导系统
1.
Review on Alignment of Ship-launched Weapon INS;
舰载武器惯导系统对准综述
2.
Nonlinear Filtering Algorithm for INS Initial Alignment;
惯导系统初始对准的非线性滤波算法
3.
Influence of Corrective Loop Parameter′s Accuracy and Stability on INS Precision;
修正回路参数的精度与稳定性对惯导系统精度的影响
4) inertial navigation
惯导系统
1.
The thought of the approach can offer a valuable reference to the domestic people engaged in researching and manufacturing inertial navigation system.
研究了进口某型飞机通过检查飞机停放航向 ,间接判断机上惯导系统平台漂移误差大小这一方法的理论依据及其计算公式。
2.
In the improved curve fitting method,the Schuler component in velocity error was decoupled through the analysis of inertial navigation system.
改进的曲线拟合法通过对惯导系统误差模型的分析,解耦出速度误差项的舒拉部分。
3.
In order to solve the initial alignment problem of carrier-based aircraft under the large azimuth misalignment condition,the error model of transfer alignment of carrier-based aircraft inertial navigation system was built in this paper.
为解决舰载机惯导系统在大方位失准角条件下的初始对准问题,建立舰载机惯导系统传递对准误差模型。
5) INS error-correction
惯导系统误差修正
6) inertial navigation system
惯导系统;惯性导航系统
补充资料：系统校正
分子式：
CAS号：
性质：对系统进行重新设计，即改变系统的结构或在系统中引进附加装置或元件，以改变系统的全部性能使系统的性能满足要求，为此目的而在系统中引入的附加装置，称为校正装置。加进校正装置后，使原来系统的缺陷得到了补偿。
CAS号：
性质：对系统进行重新设计，即改变系统的结构或在系统中引进附加装置或元件，以改变系统的全部性能使系统的性能满足要求，为此目的而在系统中引入的附加装置，称为校正装置。加进校正装置后，使原来系统的缺陷得到了补偿。
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