Motion of an Artificial Satellite in an Eccentric Gravitation Field
Author : Vladimir Grigorʹevich Demin
Publisher :
Page : 340 pages
File Size : 49,52 MB
Release : 1970
Category : Artificial satellites
ISBN :
Author : Vladimir Grigorʹevich Demin
Publisher :
Page : 340 pages
File Size : 49,52 MB
Release : 1970
Category : Artificial satellites
ISBN :
Author : V. G Demin
Publisher :
Page : 329 pages
File Size : 49,40 MB
Release : 1968
Category :
ISBN :
Author :
Publisher :
Page : 329 pages
File Size : 24,88 MB
Release : 1970
Category : Artificial satellites
ISBN :
Author : Vladimir Grigorʹevich Demin
Publisher :
Page : 340 pages
File Size : 19,36 MB
Release : 1959
Category : Artificial satellites
ISBN :
Author :
Publisher :
Page : 324 pages
File Size : 46,10 MB
Release : 1969
Category : Artificial satellites
ISBN :
Author : William M. Kaula
Publisher :
Page : 20 pages
File Size : 49,98 MB
Release : 1962
Category : Artificial satellites
ISBN :
Mathematical developments of the gravitational effects of the sun and moon on a close satellite were made. The developments were made as a result of attempts to adapt to a form convenient in analyzing close satellite orbits for terrestrial gravitational field variations. The disturbing functions are expressed in osculating Keplerian elements for use in equations of motion. (Author).
Author : Peter Musen
Publisher :
Page : 28 pages
File Size : 37,29 MB
Release : 1961
Category : Artificial satellites
ISBN :
Author : V. F. Proskurin
Publisher :
Page : 16 pages
File Size : 41,4 MB
Release : 1960
Category : Artificial satellites
ISBN :
Author : V. L. Pisacane
Publisher :
Page : 59 pages
File Size : 25,36 MB
Release : 1974
Category :
ISBN :
The report presents the development of a solution for satellite orbits in a nonrotating atmosphere and takes into account the second through fourth zonal harmonics of the gravitational potential. It is basically an extension of Lane's work in that his power-law representation of the atmospheric density function, which implies a linear density scale height, is replaced by a density function with a quadratic density scale height. The quadratic scale height is shown to provide a substantially better fit to the atmospheric density. To integrate the equations of motion analytically, it is necessary to expand the density function in a series. Limitations which appear in the Lane and the Brouwer and Hori theories for small eccentricities, low inclinations, and critical inclinations still exist. (Modified author abstract).
Author : Abolghassem Ghaffari
Publisher :
Page : 18 pages
File Size : 18,24 MB
Release : 1970
Category : Artificial satellites
ISBN :
The Lindstedt perturbation method is applied to the motion of an artificial Earth satellite that moves along a geodesic of the Schwarzschild metric of general relativity. The purpose of this analysis is to determine the extent to which general-relativistic effects are detectable in range measurements of Earth-orbiting spacecraft.