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Titlebook: INS/CNS/GNSS Integrated Navigation Technology; Wei Quan,Jianli Li,Jiancheng Fang Book 2015 National Defense Industry Press, Beijing and Sp

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書(shū)目名稱(chēng)INS/CNS/GNSS Integrated Navigation Technology
編輯Wei Quan,Jianli Li,Jiancheng Fang
視頻videohttp://file.papertrans.cn/461/460300/460300.mp4
概述Systematically introduces key technologies for integrated navigations of INS/GNSS, INS/CNS, and INS/CNS/GNSS.Presents detailed illustrations for integrated navigation methods.Includes many examples of
圖書(shū)封面Titlebook: INS/CNS/GNSS Integrated Navigation Technology; Wei Quan,Jianli Li,Jiancheng Fang Book 2015 National Defense Industry Press, Beijing and Sp
描述.This book not only introduces the principles of INS, CNS and GNSS, the related filters and semi-physical simulation, but also systematically discusses the key technologies needed for integrated navigations of INS/GNSS, INS/CNS, and INS/CNS/GNSS, respectively. INS/CNS/GNSS integrated navigation technology has established itself as an effective tool for precise positioning navigation, which can make full use of the complementary characteristics of different navigation sub-systems and greatly improve the accuracy and reliability of the integrated navigation system. The book offers a valuable reference guide for graduate students, engineers and researchers in the fields of navigation and its control..Dr. .Wei Quan., Dr. .Jianli Li., Dr. .Xiaolin Gong .and Dr. .Jiancheng Fang .are all researchers at the Beijing University of Aeronautics and Astronautics..
出版日期Book 2015
關(guān)鍵詞CNS; Celestial Navigation; GNSS; INS; Inertial Navigation; Integrated Navigation; Semi-physical Simulation
版次1
doihttps://doi.org/10.1007/978-3-662-45159-5
isbn_softcover978-3-662-52448-0
isbn_ebook978-3-662-45159-5
copyrightNational Defense Industry Press, Beijing and Springer-Verlag Berlin Heidelberg 2015
The information of publication is updating

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Study for Real-Time Ability of INS/CNS/GNSS Integrated Navigation Method, hand, it is sometimes required to design several filters since observation information of a navigation subsystem is nonsynchronous, and the output frequency is inconsistent, which further increases the difficulty of navigation computer data processing[1–2].
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Error Modeling, Calibration, and Compensation of Inertial Measurement Unit (IMU), subject to integral operation, navigation calculation error of SINS accumulates continuously with the time, and oscillates and diverges constantly. Therefore, it is a must to understand error characteristics of SINS and conduct necessary system modeling, calibration, and compensation.
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發(fā)表于 2025-3-23 03:02:50 | 只看該作者
Filters in Navigation System,rief introduction to research results of relevant scholars at home and abroad during recent years on filter estimation method to provide basic theoretical knowledge for research contents of subsequent chapters of this book.
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發(fā)表于 2025-3-23 06:47:44 | 只看該作者
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