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Piloted simulation of one-on-one helicopter air combat at NOE flight levelsA piloted simulation designed to examine the effects of terrain proximity and control system design on helicopter performance during one-on-one air combat maneuvering (ACM) is discussed. The NASA Ames vertical motion simulator (VMS) and the computer generated imagery (CGI) systems were modified to allow two aircraft to be independently piloted on a single CGI data base. Engagements were begun with the blue aircraft already in a tail-chase position behind the red, and also with the two aircraft originating from positions unknown to each other. Maneuvering was very aggressive and safety requirements for minimum altitude, separation, and maximum bank angles typical of flight test were not used. Results indicate that the presence of terrain features adds an order of complexiaty to the task performed over clear air ACM and that mix of attitude and rate command-type stability and control augmentation system (SCAS) design may be desirable. The simulation system design, the flight paths flown, and the tactics used were compared favorably by the evaluation pilots to actual flight test experiments.
Document ID
19850018409
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Lewis, M. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Aiken, E. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
NAS 1.15:86686
AD-A160538
NASA-TM-86686
USAAVSCOM-TR-85-A-2
Report Number: NAS 1.15:86686
Report Number: AD-A160538
Report Number: NASA-TM-86686
Report Number: USAAVSCOM-TR-85-A-2
Accession Number
85N26720
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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