从工程实用和维护的角度出发，提出了一种针对机载捷联式系统的空中标定方法。
In view of engineering utility and maintenance, an in-flight calibration method for aircraft SINS was presented.
将捷联式罗经算法移植到DSP系统中加以实现，通过实验验证了整个系统算法的可行性，从而完成了捷联式光纤陀螺罗经系统的设计。
The algorithm of strapdown gyrocompass system is replanted into DSP for realization, and feasibility is validated by experiment, so the design of strapdown gyrocompass system based on FOG is finished.
论文针对使用捷联惯导系统为中制导的近距空空导弹，设计了一种基于数字信号处理器(dsp)的小型数字式捷联航姿应用系统。
A mini digital Attitude and Heading Reference System (AHRS) based on DSP is designed, which can be used on air-to-air missile with Strapdown Inertial Navigation System (SINS) as mid-course guidance.
本文提出一种把平台式和捷联式惯导系统结合在一起的新的惯性导航系统。
A new type of inertial navigation system combining customary platform type with strap-down one is put forward.
初始对准是捷联式惯导系统关键技术之一。 初始对准精度直接影响捷联式惯导系统的工作精度，初始对准时间也是反映武器系统快速反应能力的重要战术指标。
One of the key technologies of SINS is the initial alignment, whose accuracy affects the precision of SINS and whose speed effects the response rapidity of the weapon.
本论文以实际的工程为背景，主要讨论并研究了捷联式惯导系统在石油管道检测中的应用。
This paper discussed and researched strap down inertial navigation system used in rock oil pipeline detection based on project practice.
针对单一捷联式惯性导航系统无法进行长时间精确导航的难题，讨论了组合导航系统的实现方法。
SINS can hardly meet the requirements of longtime. To solve the problem of SINS, the integrated navigation system design method is studied in this paper.
惯性导航定位系统分为平台式惯导系统和捷联式惯导系统两种。
Inertial navigation system is composed of strap down inertial navigation system and platform inertial navigation system.
本文给出了捷联式惯性导航系统一种简单实用的场地标定方法。
A simple and utility field fast calibration method for the gyroflex strapdown inertial system has been presented in this paper .
本文从惯性导航基本方程出发，推导了激光陀螺捷联式惯性导航系统的系统级标定的一种误差标定模型。
In this paper, based on the inertial navigation equation, a novel model for the laser gyro strapdown inertial navigation system is provided.
本文从惯性导航基本方程出发，推导了激光陀螺捷联式惯性导航系统的系统级标定的一种误差标定模型。
In this paper, based on the inertial navigation equation, a novel model for the laser gyro strapdown inertial navigation system is provided.
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