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Autonomous Trajectory Planning and Guidance Control for Launch Vehicles

Song, Zhengyu und Zhao, Dangjun und Theil, Stephan, eds. (2023) Autonomous Trajectory Planning and Guidance Control for Launch Vehicles. Springer Series in Astrophysics and Cosmology. Springer Nature Singapore. doi: 10.1007/978-981-99-0613-0. ISBN 978-981-99-0613-0. ISSN 2731-734X.

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Offizielle URL: https://doi.org/10.1007/978-981-99-0613-0

Kurzfassung

This open access book highlights the autonomous and intelligent flight control of future launch vehicles for improving flight autonomy to plan ascent and descent trajectories onboard, and autonomously handle unexpected events or failures during the flight. Since the beginning of the twenty-first century, space launch activities worldwide have grown vigorously. Meanwhile, commercial launches also account for the booming trend. Unfortunately, the risk of space launches still exists and is gradually increasing in line with the rapidly rising launch activities and commercial rockets. In the history of space launches, propulsion and control systems are the two main contributors to launch failures. With the development of information technologies, the increase of the functional density of hardware products, the application of redundant or fault-tolerant solutions, and the improvement of the testability of avionics, the launch losses caused by control systems exhibit a downward trend, and the failures induced by propulsion systems become the focus of attention. Under these failures, the autonomous planning and guidance control may save the missions. This book focuses on the latest progress of relevant projects and academic studies of autonomous guidance, especially on some advanced methods which can be potentially real-time implemented in the future control system of launch vehicles. In Chapter 1, the prospect and technical challenges are summarized by reviewing the development of launch vehicles. Chapters 2 to 4 mainly focus on the flight in the ascent phase, in which the autonomous guidance is mainly reflected in the online planning. Chapters 5 and 6 mainly discuss the powered descent guidance technologies. Finally, since aerodynamic uncertainties exert a significant impact on the performance of the ascent / landing guidance control systems, the estimation of aerodynamic parameters, which are helpful to improve flight autonomy, is discussed in Chapter 7. The book serves as a valuable reference for researchers and engineers working on launch vehicles. It is also a timely source of information for graduate students interested in the subject.

elib-URL des Eintrags:https://elib.dlr.de/194780/
Dokumentart:Lehr- oder Fachbuch
Titel:Autonomous Trajectory Planning and Guidance Control for Launch Vehicles
Datum:15 April 2023
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
DOI:10.1007/978-981-99-0613-0
Herausgeber:
HerausgeberInstitution und/oder E-Mail-Adresse der HerausgeberHerausgeber-ORCID-iDORCID Put Code
Song, ZhengyuChina Academy of Launch Vehicle Technology, Zhejiang Universityhttps://orcid.org/0000-0001-8011-4195NICHT SPEZIFIZIERT
Zhao, DangjunSchool of Automation, Central South University, ChinaNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Theil, StephanStephan.Theil (at) dlr.dehttps://orcid.org/0000-0002-5346-8091133864535
Verlag:Springer Nature Singapore
Name der Reihe:Springer Series in Astrophysics and Cosmology
ISSN:2731-734X
ISBN:978-981-99-0613-0
Status:veröffentlicht
Stichwörter:Carrier Rockets, Ascend and Descend Guidance Control, Fault Tolerant Control, Thrust Drop, Orbital Insertion, Rapid Trajectory Planning, Satellite Launch Vehicle, Reusable Rockets
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - Projekt CALLISTO [RP]
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Navigations- und Regelungssysteme
Hinterlegt von: Theil, Dr.-Ing. Stephan
Hinterlegt am:27 Apr 2023 11:33
Letzte Änderung:06 Okt 2023 11:19

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