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Propeller modulation effects on a scanning beam microwave landing systemAn investigation to assess the modulation effects on microwave signals transmitted through rotating propeller blades. Interruption of the antenna line-of-sight signal by the rotating propeller causes a variation of path loss, which produces essentially an amplitude modulation of the received signal. This interruption or blockage effect is generally only partial because of edge diffraction around the particular interfering propeller blade. Signals reflected from the rotating propeller will also cause Doppler frequency shifts to be present in the received signals. A scanning beam microwave landing system (MLS) known as MODILS (modular instrument landing system) was used to process the received signals for display. The effects of propeller modulation were studied by varying the following parameters: (1) spacing between propeller and receiving antenna, (2) propeller dimensions, (3) propeller speed (rpm), (4) number of propeller blades, (5) system data rate, (6) receiver response time, and (7) receiver antenna aperture.
Document ID
19740023504
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pope, J. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Staehle, W. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Communications
Report/Patent Number
NASA-TM-X-62368
Report Number: NASA-TM-X-62368
Accession Number
74N31617
Funding Number(s)
PROJECT: RTOP 513-53-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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