DocumentCode :
1178525
Title :
Continuous Drift Angle from a Search Radar
Author :
Longacre, A. ; Mader, G.E.
Author_Institution :
Defense Systems Laboratory, Syracuse University Research Corporation, Syracuse University, Syracuse, N. Y.
Issue :
2
fYear :
1963
fDate :
6/1/1963 12:00:00 AM
Firstpage :
93
Lastpage :
97
Abstract :
Noncoherent Doppler permits determination of the ground course as the azimuth of a null in the clutter Doppler returns and, therefore, can be a frequency insensitive adjunct to a pilotage search radar, especially where weight and/or power is at a premium. This stands in contrast to the customary coherent Doppler navigators which relate the frequency changes upon reflection, fore and aft, to the drift angle. An X-band self-coherent Doppler implementation developed that 88 per cent of the drift-angle measurement was within ± 1° of a concurrent optical measurement.
Keywords :
Airborne radar; Aircraft; Azimuth; Doppler radar; Engineering profession; Frequency; Navigation; Radar clutter; Radar tracking; Vehicles;
fLanguage :
English
Journal_Title :
Aerospace and Navigational Electronics, IEEE Transactions on
Publisher :
ieee
ISSN :
0096-1957
Type :
jour
DOI :
10.1109/TANE.1963.4502095
Filename :
4502095
Link To Document :
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