1.
Research of SINS Initial Alignment on Dynamic Base
捷联惯导系统晃动基座初始对准研究
2.
Research on ESG Strapdown System Attitude Initial Alignment
静电陀螺捷联系统姿态初始对准研究
3.
Nonlinear Filtering Algorithm for INS Initial Alignment
惯导系统初始对准的非线性滤波算法
4.
The Research of Filter Technic in Inertial Alignment of Strapdown System;
捷联惯导系统初始对准滤波技术研究
5.
Study of Alignment Techniques on the Strap-down Inertial Navigation System;
捷联惯性导航系统初始对准技术研究
6.
The Research and Design of Initial Alignment in Strapdown Inertial Navigation System;
捷联惯导系统的初始对准研究与设计
7.
Research on Initial Alignment Technique of Micro Slicon Inertial System Based on MTi
基于MTi的硅微系统初始对准技术研究
8.
Initial Alignment Method of Inclinometer Based on North Seeking Technology
基于寻北技术的测斜仪初始对准方法
9.
Research of Extended and Unscented Kalman Filtering in Initial Alignment of Inertial Navigation System
EKF和UKF在惯导初始对准中的应用研究
10.
SINS initial alignment on moving bases based on particle filter
基于PF的SINS动基座初始对准
11.
SINS Initial Alignment Based on Improved UKF
捷联惯导初始对准的UKF改进算法
12.
The Application of Simplified UKF to Initial Alignment of SINS on Swaying Base
简化UKF在SINS摇摆基座上的初始对准
13.
Initial Alignment of SINS on stationary Base Using Set-Membership Filter
基于集员滤波的SINS静基座初始对准
14.
An Initial Alignment Method of Large Azimuth Misalignment Angle in Strap-down Inertial Navigation System Based on Particle Filter
一种粒子滤波SINS大方位失准角初始对准方法
15.
Study on the Initial Alignment of INS Under Large Heading Uncertainty
惯导系统大方位失准角下的初始对准探讨
16.
3. The aim of initial alignment of SINS is to compute the initial values of Strapdown matrix.
3．捷联惯性导航系统初始对准的目的是建立捷联矩阵的初始值。
17.
The Simulation Study on the SINS Rapid Alignment Technology
捷联惯导系统快速初始对准方法仿真研究
18.
The Research of Filter Technic in Initial Alignment of INS/GPS Integrated Navigation System;
INS/GPS组合导航系统初始对准滤波方法研究