Rigid Body Dynamics for Space Applications (ePub)

Name: Rigid Body Dynamics for Space Applications
Brand: Elsevier Science & Techn.
SKU: 86111341
Price: 138.00 EUR
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(Sprache: Englisch)

Autor: Vladimir S Aslanov

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Rigid Body Dynamics for Space Applications, Vladimir S Aslanov

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Rigid Body Dynamics for Space Applications explores the modern problems of spaceflight mechanics, such as attitude dynamics of re-entry and space debris in Earth's atmosphere; dynamics and control of coaxial satellite gyrostats; deployment, dynamics, and...

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Rigid Body Dynamics for Space Applications explores the modern problems of spaceflight mechanics, such as attitude dynamics of re-entry and space debris in Earth's atmosphere; dynamics and control of coaxial satellite gyrostats; deployment, dynamics, and control of a tether-assisted return mission of a re-entry capsule; and removal of large space debris by a tether tow.

Most space systems can be considered as a system of rigid bodies, with additional elastic and viscoelastic elements and fuel residuals in some cases. This guide shows the nature of the phenomena and explains the behavior of space objects. Researchers working on spacecraft attitude dynamics or space debris removal as well as those in the fields of mechanics, aerospace engineering, and aerospace science will benefit from this book.

Provides a complete treatise of modeling attitude for a range of novel and modern attitude control problems of spaceflight mechanics
Features chapters on the application of rigid body dynamics to atmospheric re-entries, tethered assisted re-entry, and tethered space debris removal
Shows relatively simple ways of constructing mathematical models and analytical solutions describing the behavior of very complex material systems
Uses modern methods of regular and chaotic dynamics to obtain results

Autoren-Porträt von Vladimir S Aslanov

Professor Vladimir S. Aslanov graduated from the Kuibyshev Aviation Institute, Kuibyshev, USSR (KuAI) in 1972 as a specialty Aircraft Engineer. In 1974 he entered postgraduate school of the Kuibyshev Aviation Institute and in 1977 received his PhD. In the period 1978-1982 Aslanov worked as an assistant professor in the KuAI. In 1990 he defended his doctoral dissertation at the Moscow Aviation Institute, Moscow/USSR, on the motion of a rigid body in the atmosphere. Since 1989 Prof. Aslanov is the head of the Department of Theoretical Mechanics of Samara State Aerospace University, Samara, Russia. Prof. Aslanov's scientific interests are classical mechanics, nonlinear oscillations and chaotic dynamics, mechanics of space flight, dynamics of gyrostats, dynamics

of tethered satellite systems and spacecraft stability.

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Bibliographische Angaben

Autor: Vladimir S Aslanov
2017, 420 Seiten, Englisch
Verlag: Elsevier Science & Techn.
ISBN-10: 0081018746
ISBN-13: 9780081018743
Erscheinungsdatum: 22.04.2017

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Dateiformat: ePub
Größe: 36 MB
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Englisch

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