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The Post Newtonian Effects: In the Critical Inclination Problem in Artificial Satellite Theory - Softcover
Synopsis
This work deals with the critical inclination problem in artificial satellite theory and the PN effects on it. It is carried out within the domain of Hamiltonian mechanics and is expressed in terms of the Delaunay variables using a perturbation approach based on Lie series and Lie transform and it is modified to suit the application in resonance cases using the Bohlin's technique. The short and long periodic terms are eliminated, and the elements of these transformations are obtained. The secular perturbations are derived and a method is outlined for the computation of position and velocity. Near the critical inclination, the Hamiltonian is reformed so as to consider the PN terms as being of order. The modified technique is applied to perform the long period transformation near the critical inclination. The solution is expressed in terms of elliptic (and like) integrals and elliptic functions. The elements of the transformation are formed and the motion of the perigee is analyzed.
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About the Author
F. A. Abd El-Salam is a professor of space dynamics at Cairo university, Egypt, and at Taibah university, Saudi Arabia. He is interested in celestial mechanics, Artificial satellite theory, Fraction calculus application. He has about 70 scientific articles, published in international refereed journals And 10 published articles in public affairs.
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The Post Newtonian Effects
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Noor Publishing Sep 2016, 2016
ISBN 10: 3330796995
ISBN 13: 9783330796997
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -This work deals with the critical inclination problem in artificial satellite theory and the PN effects on it. It is carried out within the domain of Hamiltonian mechanics and is expressed in terms of the Delaunay variables using a perturbation approach based on Lie series and Lie transform and it is modified to suit the application in resonance cases using the Bohlin's technique. The short and long periodic terms are eliminated, and the elements of these transformations are obtained. The secular perturbations are derived and a method is outlined for the computation of position and velocity. Near the critical inclination, the Hamiltonian is reformed so as to consider the PN terms as being of order. The modified technique is applied to perform the long period transformation near the critical inclination. The solution is expressed in terms of elliptic (and like) integrals and elliptic functions. The elements of the transformation are formed and the motion of the perigee is analyzed. 196 pp. Englisch. Seller Inventory # 9783330796997
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The Post Newtonian Effects
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Condition: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Abd El-Salam FawzyF. A. Abd El-Salam is a professor of space dynamics at Cairo university, Egypt, and at Taibah university, Saudi Arabia. He is interested in celestial mechanics, Artificial satellite theory, Fraction calculus applica. Seller Inventory # 151242650
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The Post Newtonian Effects : In the Critical Inclination Problem in Artificial Satellite Theory
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - This work deals with the critical inclination problem in artificial satellite theory and the PN effects on it. It is carried out within the domain of Hamiltonian mechanics and is expressed in terms of the Delaunay variables using a perturbation approach based on Lie series and Lie transform and it is modified to suit the application in resonance cases using the Bohlin's technique. The short and long periodic terms are eliminated, and the elements of these transformations are obtained. The secular perturbations are derived and a method is outlined for the computation of position and velocity. Near the critical inclination, the Hamiltonian is reformed so as to consider the PN terms as being of order. The modified technique is applied to perform the long period transformation near the critical inclination. The solution is expressed in terms of elliptic (and like) integrals and elliptic functions. The elements of the transformation are formed and the motion of the perigee is analyzed. Seller Inventory # 9783330796997
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The Post Newtonian Effects: In the Critical Inclination Problem in Artificial Satellite Theory
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Paperback. Condition: Brand New. 196 pages. 8.66x5.91x0.45 inches. In Stock. Seller Inventory # 3330796995
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The Post Newtonian Effects
Published by
Noor Publishing Sep 2016, 2016
ISBN 10: 3330796995
ISBN 13: 9783330796997
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Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germany
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Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -This work deals with the critical inclination problem in artificial satellite theory and the PN effects on it. It is carried out within the domain of Hamiltonian mechanics and is expressed in terms of the Delaunay variables using a perturbation approach based on Lie series and Lie transform and it is modified to suit the application in resonance cases using the Bohlin's technique. The short and long periodic terms are eliminated, and the elements of these transformations are obtained. The secular perturbations are derived and a method is outlined for the computation of position and velocity. Near the critical inclination, the Hamiltonian is reformed so as to consider the PN terms as being of order. The modified technique is applied to perform the long period transformation near the critical inclination. The solution is expressed in terms of elliptic (and like) integrals and elliptic functions. The elements of the transformation are formed and the motion of the perigee is analyzed.Books on Demand GmbH, Überseering 33, 22297 Hamburg 196 pp. Englisch. Seller Inventory # 9783330796997
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The Post Newtonian Effects | In the Critical Inclination Problem in Artificial Satellite Theory
Seller: preigu, Osnabrück, Germany
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Taschenbuch. Condition: Neu. The Post Newtonian Effects | In the Critical Inclination Problem in Artificial Satellite Theory | Fawzy Abd El-Salam | Taschenbuch | 196 S. | Englisch | 2016 | Noor Publishing | EAN 9783330796997 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. Seller Inventory # 102880183