DocumentCode :
952525
Title :
Comparison of Precalculated Orbital Elements of the Army Explorer Satellites with the Actual Elements Derived from Observations
Author :
Krause, H.G.L. ; DeWitt, R.N.
Author_Institution :
Future Projects Design Branch, Structures and Mechanics Lab., U. S. Army Ballistic Missile Agency, Redstone Arsenal, Ala.
Issue :
42403
fYear :
1960
Firstpage :
345
Lastpage :
354
Abstract :
Based on precalculated data for the position and velocity vector of the injection points for the Explorers I through V, orbital elements are derived and compared with the actual orbital elements at injection time, calculated from position and velocity data obtained from radar measurements. Calculations are also made for the different orbital periods of a satellite perturbed by the Earth´s oblateness. For Explorer I, it is shown that the actual orbital elements derived from tracking observations agree well with the actual elements derived from early astronomical observations.
Keywords :
Artificial satellites; Differential equations; Earth; Military satellites; Missiles; Orbital calculations; Radar measurements; Radar tracking; Rockets; Spaceborne radar;
fLanguage :
English
Journal_Title :
Military Electronics, IRE Transactions on
Publisher :
ieee
ISSN :
0096-2511
Type :
jour
DOI :
10.1109/IRET-MIL.1960.5008247
Filename :
5008247
Link To Document :
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