Author: Jean E. BrittonPublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 114
Book Description
Perturbative Forces Affecting the Motion of Artificial Earth Satellites
Author: Jean E. BrittonPublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 114
Book Description
First-order Perturbations in the Motion of Earth Satellites Due to Oblateness of the Earth
Author: V. F. ProskurinPublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 16
Book Description
Perturbations of Orbits of Artificial Satellites Due to Air Resistance
Author: I͡U. V. BatrakovPublisher:
ISBN:
Category : Air resistance
Languages : en
Pages : 18
Book Description
Motion of an Artificial Satellite in an Eccentric Gravitation Field
Author: Vladimir Grigorʹevich DeminPublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 340
Book Description
Integration of the Relativistic Equations of Motion of an Artificial Earth Satellite
Author: Abolghassem GhaffariPublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 18
Book Description
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.
Perturbation of the First Order in the Motion of an Artificial Satellite Caused by the Oblateness of the Earth
Author: V. F. ProskurinPublisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
The motion of the satellite and the gravitational field of an oblate planet is considered under the assumptions that the inclination of the orbit may be arbitrary, that the planet has the form of a smooth ellipsoid of revolution, and that the polar compression is small enough so that the expansion of the perturbation function can be restricted to the first degree term. The perturbation function is expanded into a power series in terms of the eccentricity; the coefficients of this series are expressed quite simply in terms of trigonometric functions of the angle of inclination. The integration of the ordinary Lagrange equations yield analytic expressions of the first order perturbations of the orbital elements in terms of the compression of the planet. The precision is up to the fourth power of the eccentricity. (Author).
Motion of Artificial Satellites in the Earth's Gravitational Field
Author: Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 322
Book Description
Development of the Lunar and Solar Perturbations in the Motion of an Artificial Satellite
Author: Peter MusenPublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 52
Book Description
Lunar and solar perturbation influence on motion of artificial satellites, and computations of satellite perturbations for Vanguard I and Explorer VI satellites.
The Motion of a Charged Satellite in the Earth's Magnetic Field
Author: L. SehnalPublisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 42
Book Description
Author: V. F. Proskurin