1) rate strapdown inertial navigation system
速率捷联惯导系统
1.
Focused on the ballistic missile using inertial guidance,the calculation and compensation for instrument error of rate strapdown inertial navigation system was researched.
针对采用惯性制导的弹道导弹,开展速率捷联惯导系统工具误差计算与补偿研究。
3) SINS
[英][sin] [美][sɪn]
捷联惯导系统
1.
A Fast Method for SINS Initial Alignment of AUV on a Locomotive Base;
一种AUV捷联惯导系统动基座快速初始对准方法
2.
Formation mechanism for static conning motion of mechanically dithered ring laser gyro SINS;
机抖激光捷联惯导系统静态圆锥运动形成机理
3.
Swing Error Compensation in Coarse Alignment for Land SINS;
车载捷联惯导系统粗对准中摆动误差补偿研究
4) Strapdown inertial navigation system
捷联惯导系统
1.
New coning error compensation algorithm of strapdown inertial navigation system;
一种新的捷联惯导系统圆锥误差补偿算法
2.
Error characteristic analysis of strapdown inertial navigation system;
捷联惯导系统误差特点分析
3.
The Research of Key Technique of FOG Strapdown Inertial Navigation System Based on DSP;
基于DSP的光纤陀螺捷联惯导系统关键技术研究
5) strapdown inertial navigation system(SINS)
捷联惯导系统
1.
By analysing systematically from theoretical point of viewing the installation error in strapdown inertial navigation system(SINS),the system s error model when there are both position-installing error and angle-installing error is concluded,and the influence on SINS s accuracy caused by installation error is simulat.
针对捷联惯导系统(SINS)中的机载安装误差进行了深入全面的研究,推导出角安装误差和位置安装误差同时存在时系统的误差模型,并对机载安装误差给导航系统精度带来的影响进行了系统仿真。
2.
Based on the characteristics of shipbased weapons,an error model of strapdown inertial navigation system(SINS) is established on a swaying base,and an autonomous initial alignment method of shipbased weapons is analyzed in details.
基于舰载武器特点,建立了捷联惯导系统(SINS)在摇摆基座下的误差模型,详细分析了一种舰载武器的自主式初始对准方案,在传统反求杆臂长度补偿杆臂效应方法的基础上,提出了一种新的补偿杆臂效应的方法,并通过仿真验证表明,该方法比传统的杆臂长度补偿法具有更高的精度,研究结果可为舰载武器对准方案的选择与设计提供理论依据。
3.
Based on the fact that it is very difficult to improve the autonomous alignment accuracy of strapdown inertial navigation system(SINS),an error function for static-state initial alignment of SINS is built.
针对目前提高捷联惯导系统自对准精度难度大这一情况,在建立SINS静基座初始对准的误差方程的基础上,通过对影响对准精度的误差因素进行分析,提出了一种在载体内部安装高精度自主寻北装置的方法,该方法可有效地提高初始对准精度。
6) strapdown inertial navigation system(SINS)
捷联惯导系统(SINS)
补充资料：惯力
1.由于惯性的作用而产生的冲力。
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