1) INS
惯导
1.
Design and Simulation of INS Attitude Correct System Based on Magnetometer;
基于磁力仪的惯导姿态校正系统设计与仿真
2.
Research on Using Imaging Seeker to Improve INS of Air-to-ground Missile;
利用成像导引头修正空地导弹惯导误差研究
3.
Development of the Correction on Airborne INS Equipment of an Airplane by GNSS;
GNSS校正某型飞机惯导系统机载设备研制
2) inertial navigation
惯导
1.
Theory, operating features and interface relations of three correction modes for the inertial navigation; Short-Range Radio Navigation, Long-Range Radio Navigation and Visual, are presented.
从校正方式组成及原理入手,详细地介绍了某型飞机导航系统惯导几种校正方式的使用特点及相互交联关系。
2.
The development situation at home and abroad (China, USA, Russia) of the "Birdcage" in the precision centrifuge used for inertial navigation is introduced in detail.
详细介绍了国内外(中、美、俄)惯导用中型精密离心机“鸟笼”的发展现状,在此基础上,对我国现阶段研制的“鸟笼”与美国的两代“鸟笼”进行了比较分析,认为我国 “鸟笼” 现阶段的研制处于国际先进水平。
3.
This paper aimed at the problem of real time processing for the simulation of inertial navigation system,A method which carries out the real time processing in the Windows 9x system is proposed-Using the VxD to acquire real time clock interrupts.
文中针对某型惯导仿真系统数据实时处理中对严格定时等问题,提出了一种在Windows9x平台下实现实时处理的方案一利用VxD获取系统时钟中断。
3) inertial navigation system
惯导
1.
The identification of nonlinearity and chaos in data obtained by ship inertial navigation system;
船舶运动惯导实测数据的非线性混沌特性的判定
2.
In this paper surrogate-data method of phase-randomized based on correlation dimension is proposed to identify the nonlinearity and chaos of data obtained by ship inertial navigation system.
利用基于关联维数的相位随机化的替代数据法,给出了对船舶运动惯导实测时间序列进行非线性判定和混沌判定的方法。
4) inertial navigation
惯导;惯性导航
5) inertial navigation
惯性导航
1.
The design and realization of a solid-state 2-D inertial navigation system;
一种固态二维惯性导航系统的设计与实现
2.
Initial alignment of inertial navigation based on support vector machine;
基于支持向量机的惯性导航初始对准
3.
Principle error analysis of inertial navigation;
基于地理坐标系的惯性导航原理性误差分析
6) 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
补充资料：惯狎
1.犹亲近。
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