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Propeller modulation effects on a scanning-beam microwave landing systemThe results of a systems study and ground test of the effects of propeller modulation on a time-multiplexed, scanning-beam microwave landing system (MLS) are presented. Propeller modulation effects are analyzed in terms of spacing between receiving antenna and propeller, propeller blade width, and propeller speed. Principal study conclusions: (1) scanning beam MLS is susceptible to errors due to synchronous propeller modulation; (2) the number of synchronous interference multiples increases as the number of propeller blades increases and as the data rate decreases; (3) the probability of synchronous interference decreases at higher data rates; and (4) MLS receiver susceptibility to propeller modulation depends upon the dynamic response of the receiver automatic gain control and the respective tracking loops.
Document ID
19750052589
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pope, J. M.
(NASA Ames Research Center Moffett Field, Calif., United States)
Staehle, W. N.
(NASA Ames Research Center Moffett Field, Calif.; Raytheon Co., Equipment Div., Sudbury, Mass., United States)
Date Acquired
August 8, 2013
Publication Date
April 1, 1975
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
SAE PAPER 750521
Meeting Information
Meeting: Society of Automotive Engineers, Business Aircraft Meeting
Location: Wichita, KS
Start Date: April 8, 1975
End Date: April 11, 1975
Sponsors: Society of Automotive Engineers
Accession Number
75A36661
Distribution Limits
Public
Copyright
Other

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