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Titlebook: Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle; Xuefeng Li,Fan Xu,Guoqiang Xu Book 2023 S

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書(shū)目名稱Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle
編輯Xuefeng Li,Fan Xu,Guoqiang Xu
視頻videohttp://file.papertrans.cn/825/824584/824584.mp4
概述Presents long-term experiences in launch vehicle control system design from authors.Offers concise and highly pragmatic content.Focuses on the inertial devices and power system‘s reconstruction scheme
叢書(shū)名稱Navigation: Science and Technology
圖書(shū)封面Titlebook: Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle;  Xuefeng Li,Fan Xu,Guoqiang Xu Book 2023 S
描述This book analyzes the problems to be solved urgently in the development of launch vehicle control system. The techniques of redundant Inertial Measurement Unit (IMU) reconfiguration and trajectory replanning are proposed aiming at the inertial device failures and power system failures during flight of launch vehicles, respectively. It introduces the background of redundant IMU reconfiguration and trajectory replanning technologies and models of launch vehicle dynamics and redundant strap-down IMUs. The approaches for redundant strap-down IMU fault detection, reconfiguration and trajectory replanning are proposed, putting forward a prospect for the development of launch vehicle control system. The content of this book is concise and highly pragmatic. It could serve as a reference for engineers and researchers engaged in the analysis, design and verification of launch vehicle control systems and also as a reference for graduate students and senior undergraduates majoring in navigation,guidance and control.
出版日期Book 2023
關(guān)鍵詞Launch Vehicle; Redundant Inertial Measurement Unit; IMU; Trajectory Replanning; Aerospace Technology
版次1
doihttps://doi.org/10.1007/978-981-19-4637-0
isbn_softcover978-981-19-4639-4
isbn_ebook978-981-19-4637-0Series ISSN 2522-0454 Series E-ISSN 2522-0462
issn_series 2522-0454
copyrightScience Press 2023
The information of publication is updating

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Model of Launch Vehicle Dynamics and Redundant Strapdown IMUs,olled object in this section. First, the coordinate system was defined, the force acting on the launch vehicle was analyzed, the motion equation was established, and then its dynamics was analyzed to provide the basis for trajectory re-planning. The zero error, installation error and scale factor er
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