Evolution of Motions of a Rigid Body About its Center of Mass (Record no. 81009)

000 -LEADER
fixed length control field 03564nam a22005775i 4500
001 - CONTROL NUMBER
control field 978-3-319-53928-7
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20220801222642.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 170420s2017 sz | s |||| 0|eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
ISBN 9783319539287
-- 978-3-319-53928-7
082 04 - CLASSIFICATION NUMBER
Call Number 629.1
100 1# - AUTHOR NAME
Author Chernousko, Felix L.
245 10 - TITLE STATEMENT
Title Evolution of Motions of a Rigid Body About its Center of Mass
250 ## - EDITION STATEMENT
Edition statement 1st ed. 2017.
300 ## - PHYSICAL DESCRIPTION
Number of Pages XXXVIII, 241 p. 52 illus.
505 0# - FORMATTED CONTENTS NOTE
Remark 2 The foundations of dynamics of a rigid body with a fixed point -- Motion of a rigid body by inertia. Euler's case -- Lagrange's case -- Equations of perturbed motion of a rigid body about its center of mass -- Perturbation torques acting upon a rigid body -- Motion of a satellite about its center of mass under the action of gravitational torque -- Motion of a rigid body with a cavity filled with a viscous fluid -- Evolution of rotations of a rigid body in a medium -- Motion of a rigid body with internal degrees of freedom -- Influence of the torque due to the solar pressure upon the motion of a Sun satellite relative to its center of mass -- Perturbed motions of a rigid body close to Lagrange's case.
520 ## - SUMMARY, ETC.
Summary, etc The book presents a unified and well-developed approach to the dynamics of angular motions of rigid bodies subjected to perturbation torques of different physical nature. It contains both the basic foundations of the rigid body dynamics and of the asymptotic method of averaging. The rigorous approach based on the averaging procedure is applicable to bodies with arbitrary ellopsoids of inertia. Action of various perturbation torques, both external (gravitational, aerodynamical, solar pressure) and internal (due to viscous fluid in tanks, elastic and visco-elastic properties of a body) is considered in detail. The book can be used by researchers, engineers and students working in attitude dynamics of spacecraft.
700 1# - AUTHOR 2
Author 2 Akulenko, Leonid D.
700 1# - AUTHOR 2
Author 2 Leshchenko, Dmytro D.
856 40 - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier https://doi.org/10.1007/978-3-319-53928-7
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type eBooks
264 #1 -
-- Cham :
-- Springer International Publishing :
-- Imprint: Springer,
-- 2017.
336 ## -
-- text
-- txt
-- rdacontent
337 ## -
-- computer
-- c
-- rdamedia
338 ## -
-- online resource
-- cr
-- rdacarrier
347 ## -
-- text file
-- PDF
-- rda
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace engineering.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Astronautics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mathematical physics.
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mechanics.
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Aerospace Technology and Astronautics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Mathematical Physics.
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1
-- Classical Mechanics.
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-- ZDB-2-ENG
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-- ZDB-2-SXE

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