NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Development and flight test of a helicopter, X-band, portable precision landing system conceptA beacon landing system (BLS) is being developed and flight tested as a part of NASA's Rotorcraft All-Weather Operations Research Program. The system is based on state-of-of-the-art X-band radar technology and digital processing techniques. The bLS airborne hardware consists of an X-band receiver and a small micropreocessor, installed in conjunction wht the aircraft instrument landing system (ILS) receiver. The microprocessor analyzes the X-band, BLS pulses and outputs ILS-compatible localizer and glide slope signals. Range information is obtained using an on-board weather/mapping radar in conjunction with the BLS. The ground station is an inexpensive, portable unit; it weighs less than 70 lb and can be quickly deployed at a landing site. Results from the flight-test program show that the BLS has a significant potential for providing rotorcaraft with low-cost, precision instrument approach capability in remote areas.
Document ID
19850018410
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Davis, T. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Clary, G. R.
(NASA Ames Research Center Moffett Field, CA, United States)
Chisholm, J. P.
(Sierra Nevada Corp. Reno, United States)
Macdonald, S. L.
(Sierra Nevada Corp. Reno, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-86710
NAS 1.15:86710
Report Number: NASA-TM-86710
Report Number: NAS 1.15:86710
Accession Number
85N26721
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available