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Redundant inertial measurement unit ...

Li, Xuefeng.

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Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle

Record Type:	Electronic resources : Monograph/item
Title/Author:	Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle/ by Xuefeng Li, Fan Xu, Guoqiang Xu.
Author:	Li, Xuefeng.
other author:	Xu, Fan.
Published:	Singapore :Springer Nature Singapore : : 2023.,
Description:	xi, 190 p. :ill. (some col.), digital ;24 cm.
[NT 15003449]:	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.
Contained By:	Springer Nature eBook
Subject:	Launch vehicles (Astronautics) -
Online resource:	https://doi.org/10.1007/978-981-19-4637-0
ISBN:	9789811946370

Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle
Li, Xuefeng.

Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle[electronic resource] /by Xuefeng Li, Fan Xu, Guoqiang Xu. - Singapore :Springer Nature Singapore :2023. - xi, 190 p. :ill. (some col.), digital ;24 cm. - Navigation: science and technology,v. 122522-0462 ;. - Navigation: science and technology ;v. 12..

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.

ISBN: 9789811946370

Standard No.: 10.1007/978-981-19-4637-0doiSubjects--Topical Terms:

1639991
Launch vehicles (Astronautics)

LC Class. No.: TL785.8.L3

Dewey Class. No.: 629.475

Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle
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245 1 0 $a Redundant inertial measurement unit reconfiguration and trajectory replanning of launch vehicle $h [electronic resource] / $c by Xuefeng Li, Fan Xu, Guoqiang Xu.
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300 $a xi, 190 p. : $b ill. (some col.), digital ; $c 24 cm.
490 1 $a Navigation: science and technology, $x 2522-0462 ; $v v. 12
505 0 $a 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.
520 $a 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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650 0 $a Space trajectories $x Mathematical models. $3 3626074
650 0 $a Inertia (Mechanics) $3 726189
650 1 4 $a Aerospace Technology and Astronautics. $3 928116
650 2 4 $a Engine Technology. $3 1774726
700 1 $a Xu, Fan. $3 1025212
700 1 $a Xu, Guoqiang. $3 3626072
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