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Switchable Beamwidth Monopulse Method and SystemA switchable beamwidth monopulse method and system are described. An antenna comprising a curved reflector and a first set of monopulse feeds positioned in the effective region of the airy disc of the antenna includes a second set of monopulse feeds. The second set of monopulse feeds is positioned outside the airy disc in the region of first bright airy ring. In narrow beamwidth monopulse operation, monopulse sum and difference channel patterns are obtained from the first set of feeds within the airy disc. In wide beamwidth monopulse operation, the difference channel pattern is obtained from the second set of feeds in the airy ring; the sum channel pattern is obtained by attenuation and phase shifting the sum channel signal obtained from the first set of feeds, and adding the resultant to the sum channel signal obtained from the second set of feeds. In a simplified form of the invention, the difference channel patterns for both narrow and wide beamwidth mode operation are obtained from the second set of feeds, while the sum channel patterns are obtained as described above.
Document ID
19760020384
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Deerkoski, L. F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Schmidt, R. F.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 8, 2013
Publication Date
June 22, 1976
Subject Category
Electronics And Electrical Engineering
Accession Number
76N27472
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-PATENT-3,965,475|NASA-CASE-GSC-11924-1
Patent Application
US-PATENT-APPL-SN-582318
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