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An Overview Of Orbital Mechanics & Astrodynamics: The Mathematics Of Simul...
US $12,00
CircaEUR 10,36
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Libro che non sembra nuovo ed è già stato letto, ma è in condizioni eccellenti. Nessun danno evidente alla copertina, dotato di sovraccoperta(se applicabile) per le copertine rigide. Nessuna pagina mancante o danneggiata, piegata o strappata, nessuna sottolineatura/evidenziazione di testo né scritte ai margini. Potrebbe presentare minimi segni identificativi sulla copertina interna. Mostra piccolissimi segni di usura. Per maggiori dettagli e la descrizione di eventuali imperfezioni, consulta l'inserzione del venditore.
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Spedizione:
US $5,22 (circa EUR 4,51) USPS Media MailTM.
Oggetto che si trova a: Washington, District Of Columbia, Stati Uniti
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Consegna prevista tra il gio 7 ago e il mar 12 ago a 94104
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Numero oggetto eBay:177137893135
Specifiche dell'oggetto
- Condizione
- ISBN
- 9781535295727
Informazioni su questo prodotto
Product Identifiers
Publisher
CreateSpace
ISBN-10
1535295724
ISBN-13
9781535295727
eBay Product ID (ePID)
234627123
Product Key Features
Book Title
Overview of Orbital Mechanics and Astrodynamics : The Mathematics of Simulating and Maneuvering Objects in Orbit
Number of Pages
324 Pages
Language
English
Topic
Physics / General
Publication Year
2016
Genre
Science
Format
Trade Paperback
Dimensions
Item Height
0.7 in
Item Weight
32.9 Oz
Item Length
11 in
Item Width
8.5 in
Additional Product Features
Intended Audience
Trade
TitleLeading
An
Synopsis
In this 'information age' satellites are playing an increasingly important role in everything from communication and navigation to the military and weather. The command and control of satellites is based on the work of Johannes Kepler (1571-1630) and the science that evolved from his fundamental theories.The physics involved in the command and control of satellites is usually categorized as orbital mechanics. Orbital mechanics is based on the desire to predict the path of a satellite in it's orbit around the earth.One of the first requirements is to develop a co-ordinate system that is easy to use and measure and defines the motion of body or satellite in its orbit.After this is accomplished the propagation of the orbital path needs to be calculated. There are numerous ways to do this. A seminal work in this procedure is "Fundamentals of Astrodynamics" by Bate, Mueller & White and "Methods of Orbit Determination" by Escobal.The next problem to address are the numerous perturbation effects. The most prominent of these effects are due to the fact that the earth is not a perfect sphere (it is oblate), the moons orbit produces a periodically disruptive effect on the orbiting body; atmospheric drag, solar radiation pressure and the precession of the earth about its axis also alter the theoretical orbit. Relativistic effects play a role in the station-keeping of the satellite as do all the above perturbations.The next step in the command and control of the satellite involves the dynamics of space flight and the mechanics of maneuvering a body in orbit by means of thrust vectors, calculating delta-v requirements.This book outlines the unclassified methods of calculating and controlling the orbits of satellites.This book is designed to be a reference and provide an overview of the topic and give the reader a structured knowledge to familiarize yourself with the topic at the most affordable price possible.The accuracy and knowledge is of an international viewpoint as the edited articles represent the inputs of many knowledgeable individuals and some of the most current knowledge on the topic, based on the date of publication., In this 'information age' satellites are playing an increasingly important role in everything from communication and navigation to the military and weather. The command and control of satellites is based on the work of Johannes Kepler (1571-1630) and the science that evolved from his fundamental theories. The physics involved in the command and control of satellites is usually categorized as orbital mechanics. Orbital mechanics is based on the desire to predict the path of a satellite in it's orbit around the earth. One of the first requirements is to develop a co-ordinate system that is easy to use and measure and defines the motion of body or satellite in its orbit. After this is accomplished the propagation of the orbital path needs to be calculated. There are numerous ways to do this. A seminal work in this procedure is "Fundamentals of Astrodynamics" by Bate, Mueller & White and "Methods of Orbit Determination" by Escobal. The next problem to address are the numerous perturbation effects. The most prominent of these effects are due to the fact that the earth is not a perfect sphere (it is oblate), the moons orbit produces a periodically disruptive effect on the orbiting body; atmospheric drag, solar radiation pressure and the precession of the earth about its axis also alter the theoretical orbit. Relativistic effects play a role in the station-keeping of the satellite as do all the above perturbations. The next step in the command and control of the satellite involves the dynamics of space flight and the mechanics of maneuvering a body in orbit by means of thrust vectors, calculating delta-v requirements. This book outlines the unclassified methods of calculating and controlling the orbits of satellites. This book is designed to be a reference and provide an overview of the topic and give the reader a structured knowledge to familiarize yourself with the topic at the most affordable price possible. The accuracy and knowledge is of an international viewpoint as the edited articles represent the inputs of many knowledgeable individuals and some of the most current knowledge on the topic, based on the date of publication.
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