NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
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, has been 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 derivation. 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
19850008512
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bull, J. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Clary, G. R.
(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. Reno, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1984
Publication Information
Publication: AGARD Helicopter Guidance and Control Systems for Battlefield Support
Subject Category
Aircraft Instrumentation
Accession Number
85N16821
Distribution Limits
Public
Copyright
Other
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available