inertial navigation system
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英
- 網絡慣性導航系統；慣性導航系統慣導系統；慣性導航裝置
例句
The attitude solution for carrier is one of the key technologies for precision navigation of Strapdown Inertial Navigation System(SINS).
載體的姿態解算算法是實現捷聯式慣性導航系統精確導航的核心技術之一。
The simulation results indicate that the calibration can compensate the error and improve the precision of the inertial navigation system.
仿真結果表明，該標定方法能夠對誤差進行補償，進而提高慣導系統的導航精度。
Avionics systems include a highly accurate inertial navigation system in which a computer provides steering information to the pilot.
航電系統包括高度精確的慣性導航系統，它通過電腦向飛行員提供轉向信息。
Main reasons for heading effect drift of an airborne platform inertial navigation system are analyzed in this paper.
本文分析了某型機載平臺式慣性導航系統航向效應漂移產生的主要原因。
Inertial navigation system is composed of strap down inertial navigation system and platform inertial navigation system.
慣性導航定位系統分為平臺式慣導系統和捷聯式慣導系統兩種。
An online identification algorithm of odometers scale factor in land used strapdown inertial navigation system is put forward.
提出陸用捷聯慣導系統中里程計刻度因子的在線辨識算法。
In the paper, the scrolling compensation algorithm in position updating of strap down inertial navigation system is researched.
研究了高動態環境下捷聯慣導位置更新中的渦卷補償算法。
Inertial Navigation System (INS) is a important navigation system with widely application in civil and military field.
慣性導航系統（INS）是一種非常重要的導航定位系統，在民用和軍事領域有廣泛的應用。
Strapdown Inertial Navigation System (SINS) leads the trend of inertial navigation systems currently.
捷聯式慣性導航系統（SINS）是目前慣性導航技術的主要發展方向。
This paper discussed and researched strap down inertial navigation system used in rock oil pipeline detection based on project practice.
本論文以實際的工程為背景，主要討論并研究了捷聯式慣導系統在石油管道檢測中的應用。
The digital levelling and fast accurate levelling method for strap down inertial navigation system (SINS) is discussed.
討論了實現捷聯慣導系統數字調平及快速精調平的方法。
It could be used in the closed-loop simulation test of flight control system and inertial navigation system.
它可用于飛行控制系統與慣性導航系統的標定和閉環仿真實驗。
Strap down inertial navigation system is a developmental orientation of inertial technique.
捷聯式慣導系統是近年來慣性導航技術的一個發展方向。
Compared with Platform Inertial Navigation System, SINS is smaller in size, lighter in weight, more reliable and cheaper.
它與平臺式慣性導航系統相比具有體積小、重量輕、成本低、可靠性高等諸多優點。
and coning error from coning motion is an essential error source of strap down inertial navigation system(SINS).
在圓錐運動下產生的圓錐誤差是捷聯慣導系統的重要誤差源。
Initial Alignment of Inertial Navigation System Using Wavelet Neural Networks.
采用小波神經網絡的慣導系統初始對準。
Finally, the block diagram of the strap-down inertial navigation system is given .
最后給出了無陀螺捷聯慣性導航系統的框圖。
The parameter error of inertial navigation system has important effect on the precision of navigation system.
捷聯慣性導航系統誤差參數標定的準確程度對于系統的導航和定位精度具有重要影響。
An expert system is proposed to diagnose faults of platform inertial navigation system.
分析了導航系統對故障診斷的基本要求以及導航系統的故障診斷方法。
In this paper, based on the inertial navigation equation, a novel model for the laser gyro strapdown inertial navigation system is provided.
本文從慣性導航基本方程出發，推導了激光陀螺捷聯式慣性導航系統的系統級標定的一種誤差標定模型。
A new type of inertial navigation system combining customary platform type with strap-down one is put forward.
本文提出一種把平臺式和捷聯式慣導系統結合在一起的新的慣性導航系統。
The strap down inertial navigation system(SINS) in weapon system needs initial alignment before the weapon is launched.
目前遠程武器系統廣泛采用捷聯慣性導航系統，該系統在發射前要經過初始對準。
A inertial navigation system, this module includes forward back pluse signals, the gyro signal, speed pulse signal and the barometer signal.
提出了一種遞推導航方案，此方案包括了前后向信號、陀螺儀信號、速度脈沖信號以及氣壓計信號。
The method of integrated attitude determination based on inertial navigation system and star sensor is researched in this paper.
研究了利用慣性導航系統與星敏感器進行組合定姿的方法。
With the development of the ship and navigation, the inertial navigation system shows its more and more important status.
隨著船舶和航海事業的日益發展，慣性技術越來越顯示出其重要的地位。
In order to utilize it better in the new generation inertial navigation system, it is necessary to study the random error model of VBA.
為了更好地將振梁加速度計應用于新一代慣導系統中，有必要研究其隨機誤差模型。
Study of Time Synchronization of Simulation on Strapdown Inertial Navigation System
捷聯慣導系統半實物仿真試驗的時序同步研究
A Real- time Neural Network Learning Algorithm Adapt to the Initial Alignment of Inertial Navigation System
適于慣導系統初始對準的神經網絡實時算法研究
Generalized Inferential Control Strategy for Expert System and its Application in Inertial Navigation System
專家系統的廣義推理控制策略研究及其在慣導系統中的應用
Study of Self-Calibration Technique for Sensor Errors in Ring Laser Gyro Strapdown Inertial Navigation System
激光陀螺捷聯慣導系統元件誤差自標定技術
Application of Two-position Alignment Technique in Strapdown Inertial Navigation System for Land Vehicle
雙位置初始對準技術在車載捷聯慣導系統中的應用研究
Multiposition Observability Analysis of Strapdown Inertial Navigation System
捷聯慣導系統多位置可觀性分析
Initial Alignment Accuracy Analysis and Simulation of Strapdown Inertial Navigation System on a Stationary Base
捷聯慣導系統靜基座初始對準精度分析及仿真
Research on a Fast Initial Alignment Method for the Strapdown Inertial Navigation System on Stationary Base
捷聯式慣導系統靜基座快速初始對準方法的研究
Inertial Instrument Error Compensation Technology in Laser Gyro Strapdown Inertial Navigation System
激光陀螺捷聯慣性導航系統中慣性器件誤差補償技術
Study on noncommutativity errors correction algorithms of laser strapdown inertial navigation system
激光捷聯慣性導航中不可交換性誤差補償算法研究
Fast Initial Alignment and Its Errors of RLG Strapdown Inertial Navigation System for Land Vehicle
車載激光捷聯慣導系統的快速初始對準及誤差分析
Initial alignment of the inertial navigation system based on a neural network suitable for the best estimation
基于最優估計神經網絡的慣導系統初始對準研究
Coupled Vibration Characteristics of Strapdown Inertial Navigation System
捷聯慣導系統振動耦合特性研究
Application of Active Disturbance Rejection Technique in Initial Alignment of Inertial Navigation System
自抗擾控制在慣性導航系統初始對準中的應用
