Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle [electronic resource] / by Xuefeng Li, Fan Xu, Guoqiang Xu.
Tipo de material: TextoSeries Navigation: Science and Technology ; 12Editor: Singapore : Springer Nature Singapore : Imprint: Springer, 2023Edición: 1st ed. 2023Descripción: XI, 190 p. 62 illus., 4 illus. in color. online resourceTipo de contenido: text Tipo de medio: computer Tipo de portador: online resourceISBN: 9789811946370Tema(s): Aerospace engineering | Astronautics | Engines | Aerospace Technology and Astronautics | Engine TechnologyFormatos físicos adicionales: Printed edition:: Sin título; Printed edition:: Sin título; Printed edition:: Sin títuloClasificación CDD: 629.1 Clasificación LoC:TL1-4050Recursos en línea: Libro electrónicoTipo de ítem | Biblioteca actual | Colección | Signatura | Copia número | Estado | Fecha de vencimiento | Código de barras |
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Libro Electrónico | Biblioteca Electrónica | Colección de Libros Electrónicos | 1 | No para préstamo |
Acceso multiusuario
Section 1 Introduction -- Section 2 Model of Launch Vehicle Dynamics and Redundant Strapdown IMUs -- Section 3 Redundant IMU Fault Detection -- Section 4 Redundant IMU Reconfiguration -- Section 5 Trajectory Replanning.
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.
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