Hamiltonian perturbation solutions for spacecraft orbit prediction the method of Lie transforms

Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems ar...

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Bibliographic Details
Main Author: Lara, Martín
Format: eBook
Language:English
Published: Berlin ; Boston Walter de Gruyter GmbH, [2021]
Series:De Gruyter studies in mathematical physics ; v. 54.
Subjects:
Online Access:https://www.lib.tsu.ru/mminfo/2023/EBSCO/2907461.pdf
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049 |a MAIN 
100 1 |a Lara, Martín,  |9 905325 
245 1 0 |a Hamiltonian perturbation solutions for spacecraft orbit prediction  |b the method of Lie transforms  |c Martín Lara. 
264 1 |a Berlin ;  |a Boston  |b Walter de Gruyter GmbH,  |c [2021] 
300 |a 1 online resource (394 pages). 
490 1 |a De Gruyter Studies in Mathematical Physics ;  |v volume 54 
500 |a Description based upon print version of record. 
505 0 0 |t Frontmatter --  |t Preface --  |t Contents --  |t 1 Introduction --  |t Part I: Hamiltonian perturbations by Lie transforms --  |t 2 The method of Lie transforms --  |t 3 Application to integrable problems --  |t Part II: Perturbed elliptic motion: Artificial satellite theory --  |t 4 The Kepler problem --  |t 5 The main problem of the artificial satellite --  |t 6 Zonal perturbations --  |t 7 Tesseral perturbations --  |t 8 Lunisolar perturbations --  |t 9 Non-conservative effects --  |t Part III: Relative motion and perturbed non-Keplerian motion --  |t 10 The Hill problem --  |t 11 Motion inside Hill's sphere --  |t 12 Motion about the libration points --  |t 13 Quasi-satellite orbits --  |t Bibliography --  |t Index 
520 |a Analytical solutions to the orbital motion of celestial objects have been nowadays mostly replaced by numerical solutions, but they are still irreplaceable whenever speed is to be preferred to accuracy, or to simplify a dynamical model. In this book, the most common orbital perturbations problems are discussed according to the Lie transforms method, which is the de facto standard in analytical orbital motion calculations. 
588 |a Description based on online resource; title from digital title page (viewed on June 01, 2021). 
504 |a Includes bibliographical references and index. 
653 0 |a Orbital mechanics  |x Mathematics.  |9 905326 
653 0 |a Perturbation (Mathematics)  |9 905327 
653 4 |a Hamilton-Jacobi-Differentialgleichung.  |9 905328 
653 4 |a Störungstheorie.  |9 905329 
653 4 |a Umlaufbahn.  |9 905330 
653 7 |a SCIENCE / Space Science.  |2 bisacsh  |9 905331 
655 4 |a EBSCO eBooks 
776 0 8 |i Print version:  |a Lara, Martín  |t Hamiltonian Perturbation Solutions for Spacecraft Orbit Prediction  |d Berlin/Boston : Walter de Gruyter GmbH,c2021 
830 0 |a De Gruyter studies in mathematical physics ;  |v v. 54.  |9 435593 
856 4 0 |u https://www.lib.tsu.ru/mminfo/2023/EBSCO/2907461.pdf 
856 |y Перейти в каталог НБ ТГУ  |u https://koha.lib.tsu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=1010754 
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