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Development and flight test of a helicopter compact, portable, precision landing system conceptAn airborne, radar-based, precision approach concept is being developed and flight tested as a part of NASA's Rotorcraft All-Weather Operations Research Program. A transponder-based beacon landing system (BLS) applying state-of-the-art X-band radar technology and digital processing techniques, was built and is being flight tested to demonstrate the concept feasibility. The BLS airborne hardware consists of an add-on microprocessor, installed in conjunction with the aircraft weather/mapping radar, which analyzes the radar beacon receiver returns and determines range, localizer deviation, and glide-slope deviation. The ground station is an inexpensive, portable unit which can be quickly deployed at a landing site. Results from the flight test program show that the BLS concept has a significant potential for providing rotorcraft with low-cost, precision instrument approach capability in remote areas.
Document ID
19840016498
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Clary, G. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Bull, J. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Davis, T. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Chisholm, J. P.
(Sierra Nevada Corp.)
Date Acquired
September 4, 2013
Publication Date
April 1, 1984
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
NAS 1.15:85951
NASA-TM-85951
A-9729
Report Number: NAS 1.15:85951
Report Number: NASA-TM-85951
Report Number: A-9729
Accession Number
84N24566
Funding Number(s)
PROJECT: RTOP 532-01-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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