The inertial navigation technology includes platform inertial navigation system and SINS.
包括平台式惯导系统和捷联惯导系统。
The drift performance of IFOG must be improved in order to apply IFOG to inertial navigation.
为了把IFOG应用于惯性导航领域，必须改善其漂移特性。
The principle of equivalence is of critical importance in our analysis of inertial navigation.
等效原理在惯性导航分析中特别重要。
Strapdown inertial navigation technology has been widely used in military and national production.
捷联惯导技术在军事和国民生产诸多领域有着广泛的应用。
This area of study is central to the technology of inertial navigation and gyroscopic stabilization.
这个研究领域是惯性导航和陀螺稳定器技术的核心。
Linear and nonlinear error models for Inertial Navigation System (INS) initial alignment are established.
建立了惯导系统(INS)初始对准的线性和非线性误差模型。
This paper presents a new continuous self-calibration and alignment technology of inertial navigation platform.
提出了一种新的惯导误差系数标定方法———连续自标定自对准方法。
The results show that gravity disturbance vector is a major error source for high accuracy inertial navigation system.
结果表明，不确定的重力扰动向量是高精度惯导系统的一个重要误差源。
In this paper, the parameter identification technique of inertial navigation platform drifting error model is studied.
本文研究了惯导平台漂移误差模型的参数辨识技术。
The scale-factor error of inertia component is greatly influential to the precision of Inertial Navigation System (INS).
在惯性导航系统中，惯性元件的标度因数误差对系统的误差产生了极大的影响。
Inertial navigation system is composed of strap down inertial navigation system and platform inertial navigation system.
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。
An online identification algorithm of odometer's scale factor in land used strapdown inertial navigation system is put forward.
提出陆用捷联惯导系统中里程计刻度因子的在线辨识算法。
Because of these advantages of SINS system, it is on the trend of replacing flat inertial navigation system in many applications.
由于捷联惯导系统具有的一系列优点，在许多应用中有取代平台式惯导系统的趋势。
The TNL-16GI is a new member of TAMAM's TNL-16 Airborne Inertial Navigation Systems family, based on proven products and technology.
TNL-16GI是TAMAM部门TNL-16机载惯性导航系统家族的新成员，基于成熟的产品和技术。
Avionics systems include a highly accurate inertial navigation system in which a computer provides steering information to the pilot.
航电系统包括高度精确的惯性导航系统，它通过电脑向飞行员提供转向信息。
Quaternion method, which has been successfully applied to the Strapdown Inertial Navigation and Guidance for tens year, is classical.
数十年来，四元数及其解法成功地应用于捷联惯性导航和制导系统中，成为经典的算法。
In this paper, an engineering example of drift error parameter identification for a type of inertial navigation platform is presented.
本文给出了某型号惯导平台漂移误差参数辨识的一个工程实例。
A new approach to transfer alignment for the initial alignment of Strapdown inertial navigation systems on moving base was put forward.
针对捷联惯导系统的动基座初始对准问题，提出了一种新的动基座快速传递对准方案。
At appraising the reliability of the missile-borne strapdown inertial navigation system, the reliability information for the key groups are needed.
在评价弹用捷联惯导系统的可靠性时，需要其关键件的可靠性信息。
Now the main navigation means of such vehicles still adopts inertial navigation, and intermediate navigation adopts terrain contour matching method.
该类飞行器目前仍采用惯性导航为主要的导航手段，中制导采用地形匹配。
Briefly the paper introduces a new method to make a DEM by a airborne laser radar combining with Global Positioning System and Inertial navigation technology.
主要介绍了利用机载激光雷达并结合全球卫星定位系统、惯性导航技术建立地形高程模型的一种新方法。
According to random vibration theory, the concentrated parameter analysis model of INS (Inertial Navigation System) absorber for random vibration is presented.
利用随机振动理论，建立了惯导减振系统的集中参数分析模型。
Active Radar Seeker (ARS) provides accurate and stable velocity information, thus possesses the possibility of gimbaled inertial navigation system (GINS) aiding.
主动雷达导引头可提供精确且稳定的测速信息，具有辅助惯导的潜力。
The error accumulation of inertial navigation system can be restrained via OD, however, OD scale factor error has remarkable effect on the positioning precision.
利用里程仪可以抑制惯导的误差积累，但里程仪刻度系数误差对组合系统的定位精度影响很大，必须对其进行校正。
Global positioning system real time kinematic technology (GPS RTK) was applied to the error model identification of the inertial navigation platform in this paper.
对在惯导平台车载试验误差模型辨识中使用全球卫星定位系统(GPS)载波相位差分(rtk)法进行了研究。
So-called GFSINS (gyroscope free strapdown inertial navigation system) is a kind of strapdown inertial navigation system with only accelerometers but no gyroscope.
无陀螺捷联惯导系统就是惯性元件只用加速度计，而不用陀螺的惯导系统。
From the system observability analysis, adding more kinds of external measurements into the inertial navigation system can enhance estimation accuracy of INS error.
通过对INS误差可观测性分析，可以看出增加不同种类的外部导航信息观测量，将有效提高INS误差修正能力。
The proposed inertial navigation course is traceable, so that the current position can be calculated again after the precision alignment to get more accurate position.
所提出的惯性导航过程是可回溯的，因而在精对准后可以重新计算当前位置，以得到更精确的当前位置。
The proposed inertial navigation course is traceable, so that the current position can be calculated again after the precision alignment to get more accurate position.
所提出的惯性导航过程是可回溯的，因而在精对准后可以重新计算当前位置，以得到更精确的当前位置。
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