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- The initial alignment and calibration of strapdown inertial system on a rocking base are investigated. 研究摇摆基座上捷联惯性导航系统的初始对准技术。
- The Application of Gyro-Free Strapdown Inertial System to the Attitude testing of Flying Objects 无陀螺捷联惯性系统对导弹姿态测试的应用
- Data Analysis and Temperature Modeling of Gyroscope in Strapdown Inertial System 捷联式惯性系统陀螺仪数据分析与温度建模
- 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。
- An independently integrated navigation system using odometer (OD) to assist the strapdown inertial navigation system (SINS/OD) is discussed. 摘要利用里程计辅助捷联惯导系统构成一种完全自主式的车载组合导航系统。
- Error Analysis and Simulation of Ring Laser Gyro Strapdown Inertial Navigation System[J]. 引用该论文 吉翠萍;陈勇;雷宏杰;韩宗虎;陈林峰.
- Myeong-Jong Yu.Equivalent error models of strapdown inertial navigation system[M].AIAA 297-3563. 谷宏强;马立元;郭利.;速率捷联惯性测量系统的数学模型及误差标定[J]
- Chen Zhe. Strapdown inertial navigation systerm theory [ M ]. 陈哲.;捷联惯性导航系统原理[M]
- The digital levelling and fast accurate levelling method for strapdown inertial navigation system (SINS) is discussed. 讨论了实现捷联惯导系统数字调平及快速精调平的方法。
- Taking advantage of this property,we designed a sort of attitude algorithm for strapdown inertial navigation system. 本文根据这一特点，设计了一种捷联惯导系统姿态算法，在圆锥补偿获得相同精度的情况下，它的计算量较少。
- Firstly, the paper introduced the basic theory and characteristics of the Strapdown Inertial Navigation System (SINS), the GPS, and the DVL system. 论文首先介绍了捷联式惯性导航系统、GPS导航系统和多普勒计程仪的基本原理及各自特点，并建立了捷联惯性导航系统的非线性误差模型。
- In the paper, the scrolling compensation algorithm in position updating of strapdown inertial navigation system is researched. 研究了高动态环境下捷联惯导位置更新中的涡卷补偿算法。
- Using Eulerian angle information in rudder-control-loop is a general method in the strapdown inertial navigation system(SINS) of aerocraft. 在舵偏控制回路中使用欧拉角姿态信息,是现有飞行器捷联惯导系统普遍采用的方法。
- Abstract： Three analytic coarse alignment methods to strapdown inertial navigation system are compared via error analysis. 摘 要： 通过误差分析对三种捷联惯导系统解析粗对准方法进行了比较。
- The mechanical dithering of ring laser gyro (RLG) brings pseudo coning motion for strapdown inertial navigation system (SINS) with dithered RLG. 摘要对于机抖激光陀螺捷联惯导系统，激光陀螺的机械抖动偏频引入伪圆锥运动。
- Abstract: In the gyroscopefree strapdown inertial navigati on system,theangularvelocity calculation precision is a key technical p oint. 文摘:在无陀螺捷联惯导系统中，角速度的解算精度是技术关键[1]。
- In the gyroscopefree strapdown inertial navigati on system,theangularvelocity calculation precision is a key technical p oint. 在无陀螺捷联惯导系统中，角速度的解算精度是技术关键[1]。
- An aircraft gaining speed during take-off is evidently not an inertial system. 一架正在加速起飞的飞机，显然不是惯性系统。
- strapdown inertial system 捷联导航系统
- strapdown inertial systems 捷联惯导系统
