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。
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。
The design of gyroscope data acquisition system for Marine strapdown inertial navigation system is presented.
介绍了船用捷联惯性导航系统中陀螺仪数据采集系统的设计。
A new type of inertial navigation system combining customary platform type with strap-down one is put forward.
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。
Main reasons for heading effect drift of an airborne platform inertial navigation system are analyzed in this paper.
文中分析了某型平台式惯性导航系统航向漂移产生的主要原因。
Inertial navigation system (INS) is a important navigation system with widely application in civil and military field.
惯性导航系统(INS)是一种非常重要的导航定位系统，在民用和军事领域有广泛的应用。
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。
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。
Compared with Platform Inertial Navigation System, SINS is smaller in size, lighter in weight, more reliable and cheaper.
它与平台式惯性导航系统相比具有体积小、重量轻、成本低、可靠性高等诸多优点。
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。
This paper describes the inertial navigation system developed in recent years at the Navigation & Automatic control laboratory.
本文介绍的这种新型惯性导航系统是我们研究室近年来所获得的研究成果。
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。
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。
This paper discussed and researched strap down inertial navigation system used in rock oil pipeline detection based on project practice.
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。
It is an effective way in integrated navigation by using Strapdown Inertial navigation System (SINS), GPS and Doppler Velocity Log (DVL).
利用捷联惯导(SINS)、GPS定位系统和多普勒计程仪(DVL)进行组合导航是水下运载器导航定位的有效方式。
A inertial navigation system, this module includes forward back pluse signals, the gyro signal, speed pulse signal and the barometer signal.
提出了一种递推导航方案，此方案包括了前后向信号、陀螺仪信号、速度脉冲信号以及气压计信号。
A passive location algorithm for the integrated navigation system of Beidou and inertial navigation system (INS) was put forward in this paper.
提出了一种北斗卫星定位系统和惯性导航系统的组合导航无源定位算法。
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。
The inertial navigation system (INS) and the GPS satellite navigation are two kinds of navigation system that be widely used in the modern aviation weapon.
惯性导航(INS)和全球定位导航(GPS)是现代航空武器中应用广泛的两种导航技术。
Then it shows the advantages of the circuit used in H modulation inertial navigation system, analyses the IMC model and verifies the concrete circuit scheme.
具体讨论了H调制式惯性导航设备中利用该种电路设计进行陀螺温度控制的优越性，分析了内模控制器设计的模型，并进行了方案的试验验证。
Single gyro strapdown inertial navigation system (SGSINS) has many advantages, for example, small volume, light weight, low cost, high reliability and so on.
单陀螺捷联惯导系统（SGSINS）不仅具有和经典捷联惯导系统相同的基本功能，而且有体积小、重量轻、成本低、可靠性高等优点。
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。
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。
During a transfer alignment of strapdown inertial navigation system, Kalman filter models are linear time varying system whose analysis of observability is difficult.
捷联惯导系统的卡尔曼滤波模型在传递对准时，为线性时变系统，而线性时变系统的可观测性分析比较困难。
During a transfer alignment of strapdown inertial navigation system, Kalman filter models are linear time varying system whose analysis of observability is difficult.
捷联惯导系统的卡尔曼滤波模型在传递对准时，为线性时变系统，而线性时变系统的可观测性分析比较困难。
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