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A Modified Hansen's Theory as Applied to the Motion of Artificial Satellites

Peter Musen
A Modified Hansen's Theory as Applied to the Motion of Artificial Satellites by Peter Musen PDF

Author : Peter Musen
Publisher :
Page : 52 pages
File Size : 21,25 MB
Release : 1960
Category : Artificial satellites
ISBN :

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This report presents a theory of oblateness perturbations of the orbits of artificial satellites based on Hansen's theory, with modification for adaptation to fast machine computation. The theory permits the easy inclusion of any gravitational terms and is suitable for the deduction of geo-physical and geodetic data from orbit observations on artificial satellites. The computations can be carried out to any desired order compatible with the accuracy of the geodetic parameters.

Computation of Satellite Orbits by the Hansen Method as Modified by Musen

Howard T. Phelan
Computation of Satellite Orbits by the Hansen Method as Modified by Musen by Howard T. Phelan PDF

Author : Howard T. Phelan
Publisher :
Page : 68 pages
File Size : 22,78 MB
Release : 1962
Category : Artificial satellites
ISBN :

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"This work attempts a complete exposition of the modified Hansen's theory developed by Dr. Peter Musen for analysis of the motion of an artificial satellite in the earth's gravitational field."--Preface.

Computation of Satellite Orbits by the Hansen Method as Modified by Musen

Howard T. Phelan
Computation of Satellite Orbits by the Hansen Method as Modified by Musen by Howard T. Phelan PDF

Author : Howard T. Phelan
Publisher :
Page : 68 pages
File Size : 16,96 MB
Release : 1962
Category : Aerodynamics
ISBN :

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A comprehensive description of the Hansen theory of satellite orbit calculation, as modified by Musen, is presented. The equations of the theory are developed in sufficient detail to allow the reader to relate them to fundamental laws of celestial mechanics. The physical and mathematical concepts underlying Hansen's coordinate system and auxiliary ellipse are treated. The disturbing potential function and its derivatives are developed in the derivation of equations for the perturbations in the orbit plane, as well as the perturbations of the orbit plane. The method is described for determination of the final position and velocity vectors of the real satellite and determination of the osculating elements. Finally, a brief evaluation of the theory is presented.

Index to NASA Technical Publications

United States. National Aeronautics and Space Administration
Index to NASA Technical Publications by United States. National Aeronautics and Space Administration PDF

Author : United States. National Aeronautics and Space Administration
Publisher :
Page : pages
File Size : 48,22 MB
Release : 1960-07
Category :
ISBN :

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Index of N A S A Technical Publications

United States. National Aeronautics and Space Administration
Index of N A S A Technical Publications by United States. National Aeronautics and Space Administration PDF

Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 448 pages
File Size : 32,26 MB
Release : 1960
Category :
ISBN :

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