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- Inertial Navigation Set 惯性导航设备
- Chen Zhe. Strapdown inertial navigation systerm theory [ M ]. 陈哲.;捷联惯性导航系统原理[M]
- Initial Alignment of Inertial Navigation System Using Wavelet Neural Networks. 采用小波神经网络的惯导系统初始对准。
- 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。
- 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。
- 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。
- Based on the status quo of two or more INS be equipped in naval ships, a new method of DINS (Double Inertial Navigation System) was presented. 摘要根据舰艇中一般配备两套或多套互为备份惯导系统的情况，提出了双惯导系统的阻尼新方法。
- Secondly, the principle of strap down inertial navigation for a rocket or cannon artillery is analyzed in details. 进而讨论了针对火箭炮或身管火炮的捷联惯性导航原理。
- The error models are very important in the error analysis and fault detection of inertial navigation system(INS). 论述了惯导系统 (INS)误差模型的重要作用 ,介绍了惯导误差方程推导必须遵循的步骤以及误差方程所涉及的坐标系的关系。
- Methods of error compensation for azimuth holding system in an INS (inertial navigation system) are presented. 给出了陆用惯性导航系统方位保持仪的误差补偿方法.
- The moving base initial alignment for GPS-aided RLG Strapdown Inertial Navigation Systems is introduced in this paper. 对GPS辅助下的激光陀螺捷联惯导系统的动基座初始对准进行了实验研究。
- Gimballed inertial navigation and strapped-down inertial navigation systems are compared. 研究了游动方位系惯导航的算法。
- Having the shorttime inertial navigation function is the main development trend of modern stabilized gyrocompass. 具备短期惯导功能是当今平台罗经发展的主流。
- 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]
- Main reasons for heading effect drift of an airborne platform inertial navigation systemare analyzed in this paper. 本文分析了某型机载平台式惯性导航系统航向效应漂移产生的主要原因。
- Finally, the block diagram of the strap-down inertial navigation system is given . 最后给出了无陀螺捷联惯性导航系统的框图。
- 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。
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