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A flight-test evaluation of a go-around control system for a twin engine powered-lift STOL airplaneAn automatic go-around control system was evaluated on the Augmentor Wing Jet Short Takeoff and Landing (STOL) Research Airplane (AWJSRA) as part of a study of an automatic landing system for a powered-lift STOL airplane. The results of the evaluation indicate that the go-around control system can successfully transition the airplane to a climb configuration from any initiation point during the glide-slope track or the flare maneuver prior to touchdown.
Document ID
19840003110
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Watson, D. M. (NASA Ames Research Center Moffett Field, CA, United States)
Hardy, G. H. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
October 1, 1983
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:84408
NASA-TM-84408
A-9482
Report Number: NAS 1.15:84408
Report Number: NASA-TM-84408
Report Number: A-9482
Accession Number
84N11178
Funding Number(s)
PROJECT: RTOP 533-02-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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