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- Chen Zhe. Strapdown inertial navigation systerm theory [ M ]. 陳哲.;捷聯(lián)慣性導航系統原理[M]
- Initial Alignment of Inertial Navigation System Using Wavelet Neural Networks. 采用小波神經(jīng)網(wǎng)絡(luò )的慣導系統初始對準。
- This area of study is central to the technology of inertial navigation and gyroscopic stabilization. 這個(gè)研究領(lǐng)域是慣性導航和陀螺穩定器技術(shù)的核心。
- The principle of equivalence is of critical importance in our analysis of inertial navigation. 等效原理在慣性導航分析中特別重要。
- It is an effective way in integrated navigation by using Strapdown Inertial Navigation System(SINS),GPS and Doppler Velocity Log(DVL). 利用捷聯(lián)慣導(SINS)、GPS定位系統和多普勒計程儀(DVL)進(jìn)行組合導航是水下運載器導航定位的有效方式。
- An independently integrated navigation system using odometer (OD) to assist the strapdown inertial navigation system (SINS/OD) is discussed. 摘要利用里程計輔助捷聯(lián)慣導系統構成一種完全自主式的車(chē)載組合導航系統。
- 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. 摘要根據艦艇中一般配備兩套或多套互為備份慣導系統的情況，提出了雙慣導系統的阻尼新方法。
- Secondly, the principle of strap down inertial navigation for a rocket or cannon artillery is analyzed in details. 進(jìn)而討論了針對火箭炮或身管火炮的捷聯(lián)慣性導航原理。
- The error models are very important in the error analysis and fault detection of inertial navigation system(INS). 論述了慣導系統 (INS)誤差模型的重要作用 ,介紹了慣導誤差方程推導必須遵循的步驟以及誤差方程所涉及的坐標系的關(guān)系。
- Methods of error compensation for azimuth holding system in an INS (inertial navigation system) are presented. 給出了陸用慣性導航系統方位保持儀的誤差補償方法.
- The moving base initial alignment for GPS-aided RLG Strapdown Inertial Navigation Systems is introduced in this paper. 對GPS輔助下的激光陀螺捷聯(lián)慣導系統的動(dòng)基座初始對準進(jìn)行了實(shí)驗研究。
- Gimballed inertial navigation and strapped-down inertial navigation systems are compared. 研究了游動(dòng)方位系慣導航的算法。
- Having the shorttime inertial navigation function is the main development trend of modern stabilized gyrocompass. 具備短期慣導功能是當今平臺羅經(jīng)發(fā)展的主流。
- Error Analysis and Simulation of Ring Laser Gyro Strapdown Inertial Navigation System[J]. 引用該論文 吉翠萍;陳勇;雷宏杰;韓宗虎;陳林峰.
- Myeong-Jong Yu.Equivalent error models of strapdown inertial navigation system[M].AIAA 297-3563. 谷宏強;馬立元;郭利.;速率捷聯(lián)慣性測量系統的數學(xué)模型及誤差標定[J]
- Main reasons for heading effect drift of an airborne platform inertial navigation systemare analyzed in this paper. 本文分析了某型機載平臺式慣性導航系統航向效應漂移產(chǎn)生的主要原因。
- Finally, the block diagram of the strap-down inertial navigation system is given . 最后給出了無(wú)陀螺捷聯(lián)慣性導航系統的框圖。
- The digital levelling and fast accurate levelling method for strapdown inertial navigation system (SINS) is discussed. 討論了實(shí)現捷聯(lián)慣導系統數字調平及快速精調平的方法。
- Taking advantage of this property,we designed a sort of attitude algorithm for strapdown inertial navigation system. 本文根據這一特點(diǎn)，設計了一種捷聯(lián)慣導系統姿態(tài)算法，在圓錐補償獲得相同精度的情況下，它的計算量較少。
- Firstly, the paper introduced the basic theory and characteristics of the Strapdown Inertial Navigation System (SINS), the GPS, and the DVL system. 論文首先介紹了捷聯(lián)式慣性導航系統、GPS導航系統和多普勒計程儀的基本原理及各自特點(diǎn)，并建立了捷聯(lián)慣性導航系統的非線(xiàn)性誤差模型。
