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A flight study of the use of direct-lift-control flaps to improve station keeping during in-flight refuelingTo investigate the effectiveness of fast-acting flaps as direct-lift-control (DLC) devices on a fighter airplane, the aileron servo systems of an F-100C variable-stability airplane were modified to provide symmetrical actuation of the surfaces. Initial flight tests using DLC indicated that the task of formation flying and, hence, in-flight refueling could be eased by actuating the DLC flaps through the conventional control stick, with the degree of improvement depending on the basic stability of the receiver aircraft. Results of refueling approaches and connections with U.S. Air Force tankers indicated a moderate overall improvement in vertical station-keeping performance (approximately 19 percent) and a sizeable overall decrease in receiver airplane motions and control activity (approximately 40 percent) with DLC.
Document ID
19730024237
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mcneill, W. E.
(NASA Ames Research Center Moffett Field, CA, United States)
Gerdes, R. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Innis, R. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Ratcliff, J. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1973
Subject Category
Aircraft
Report/Patent Number
A-4904
NASA-TM-X-2936
Report Number: A-4904
Report Number: NASA-TM-X-2936
Accession Number
73N32970
Funding Number(s)
PROJECT: RTOP 136-62-01-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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