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strap-down inertial navigation system
捷联式惯性导航系统
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strapdown inertial navigation equipment
捷联式惯性导航设备
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rate strapdown inertial measurement system
速率捷联惯性测量系统
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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。
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Research of SINS Initial Alignment on Dynamic Base
捷联惯导系统晃动基座初始对准研究
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Optimal Design for Sculling algorithms of SINS
捷联惯导系统划船效应补偿算法研究
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CALCULATION FOR ATTITUDE ANGLES OF AN ALL ATTITUDE AEROPLANE STRAPDOWN SYSTEM
全姿态飞机捷联式系统姿态角的计算
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Identification of Strapdown Gyroscopic Drift Model and Its Application
捷联陀螺漂移误差模型辨识及其应用
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Research on ESG Strapdown System Attitude Initial Alignment
静电陀螺捷联系统姿态初始对准研究
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A Study on the Marine Strapdown Navigation System Based on FOG;
基于光纤陀螺船用捷联导航系统研究
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Research on the Error Model of Spaceborne Fiber Optic Gyro Strapdown System;
星载光纤陀螺捷联系统误差建模研究
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Study on High-accuracy Algorithms in the SINS;
高精度捷联式惯性导航系统算法研究
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The Research of Hardware of Strapdown Inertial Navigation System Based on FOG;
光纤陀螺捷联惯导系统硬件电路研究
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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
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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
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Design of Strapdown Inertial Navigation and Control Computer Based on OMAP5912;
基于OMAP5912的捷联式制导计算机设计
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Study on Strapdown Algorithm and Its Realization by DSP under High Dynamic Environment;
高动态环境下捷联算法研究及DSP实现
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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