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Navigation Using the Transit of an Artificial Satellite
Published online by Cambridge University Press: 18 January 2010
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F. G. Smith describes (this Journal, 13, 109) a system for determining position from a single observation, probably lasting for a time of the order of a few minutes, of radio transmissions from an artificial Earth satellite. There are in this system two engineering difficulties which I think Dr. Smith has underestimated; these are the frequency stability and the power required. In order to establish these requirements it is necessary to consider in some detail how Dr. Smith's system would work.
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- Copyright © The Royal Institute of Navigation 1960
References
REFERENCES
1Lea, N. (1957). Further radio observations of the first satellite, Nature, Lond., 180, 943.CrossRefGoogle Scholar
2Stanesby, H. and others (1958). Precise frequency measurements on the first Russian satellite; Analysis of doppler data from Earth satellites and discussion, Proc. Inst. Elect. Engineers, 105B, 96–100 and 108–112.Google Scholar
3Guier, W. H. and Weiffenbach, G. C. (1960). A satellite Doppler Navigation System, Troc. Inst. Rad. Engrs., 48, 507.Google Scholar
4Ashbrook, F. M. and Stevenson, D. D. (1960). The Navy's Portable Satellite Tracking Stations, Trans. Inst. Rad. Engrs., SET-6, 41.Google Scholar
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