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Orbits: 2nd Order Singularity-free Solutions

Autor Guochang Xu, Jia Xu
en Limba Engleză Paperback – 10 iul 2015
The development of the orbits theory lags behind the development of satellite technology. This book provides, for the first time in the history of human satellite development, the complete third order solution of the orbits under all possible disturbances. It describes the theory of satellite orbits, derives the complete solutions of the orbital disturbances, describes the algorithms of orbits determination based on the theory, describes the applications of the theory to the phenomenon of the satellite formation physically. The subjects include: Orbits Motion Equations, Disturbance theory, Solutions of the differential Equations, Algorithms of Orbits determinations, Applications of the theory to the satellite formation.
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Specificații

ISBN-13: 9783642441806
ISBN-10: 3642441807
Pagini: 452
Ilustrații: XXIII, 426 p.
Dimensiuni: 155 x 235 x 24 mm
Greutate: 0.63 kg
Ediția:2nd ed. 2013
Editura: Springer Berlin, Heidelberg
Colecția Springer
Locul publicării:Berlin, Heidelberg, Germany

Public țintă

Research

Cuprins

Coordinate and Time Systems.- Keplerian Orbits.- Perturbations on the Orbits.- Solutions of C20 Perturbation.- Solutions of Geopotential Perturbations.- Solutions of Extraterrestrial Disturbances.- Numerical Orbit Determination.- Analytic Orbit Determination.- Singularity-Free Theory and Discussions.

Notă biografică

Dr. Guochang Xu, GFZ Potsdam, Germany
xu@gfz-potsdam.de

Textul de pe ultima copertă

The development of the orbits theory lags behind the development of satellite technology. This book provides, for the first time in the history of human satellite development, the complete third order solution of the orbits under all possible disturbances. It describes the theory of satellite orbits, derives the complete solutions of the orbital disturbances, describes the algorithms of orbits determination based on the theory, describes the applications of the theory to the phenomenon of the satellite formation physically. The subjects include: Orbits Motion Equations, Disturbance theory, Solutions of the differential Equations, Algorithms of Orbits determinations, Applications of the theory to the satellite formation.

Caracteristici

Provides the complete third order solution of the orbits under all possible disturbances Provides the basis for a revolution of orbits related applications The phenomenon of the satellite motion may now be more precisely described than ever before