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Ground-to-Flight Handling Qualities Comparisons for a High Performance AirplaneA flight test program was conducted in conjunction with a ground-based piloted simulation study to enable a comparison of handling qualities ratings for a variety of maneuvers between flight and simulation of a modern high performance airplane. Specific objectives included an evaluation of pilot-induced oscillation (PIO) tendencies and a determination of maneuver types which result in either good or poor ground-to-flight pilot handling qualities ratings. A General Dynamics F-16XL aircraft was used for the flight evaluations, and the NASA Langley Differential Maneuvering Simulator was employed for the ground based evaluations. Two NASA research pilots evaluated both the airplane and simulator characteristics using tasks developed in the simulator. Simulator and flight tests were all conducted within approximately a one month time frame. Maneuvers included numerous fine tracking evaluations at various angles of attack, load factors and speed ranges, gross acquisitions involving longitudinal and lateral maneuvering, roll angle captures, and an ILS task with a sidestep to landing. Overall results showed generally good correlation between ground and flight for PIO tendencies and general handling qualities comments. Differences in pilot technique used in simulator evaluations and effects of airplane accelerations and motions are illustrated.
Document ID
19970005147
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Brandon, Jay M.
(NASA Langley Research Center Hampton, VA United States)
Glaab, Louis J.
(Lockheed Engineering and Sciences Co. Hampton, VA United States)
Brown, Philip W.
(NASA Langley Research Center Hampton, VA United States)
Phillips, Michael R.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publisher: The American Inst. of Aeronautics and Astronautics
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA Paper 95-3457
NASA-TM-111925
NAS 1.15:111925
Report Number: AIAA Paper 95-3457
Report Number: NASA-TM-111925
Report Number: NAS 1.15:111925
Meeting Information
Meeting: Atmospheric Flight Mechanics
Location: Baltimore, MD
Country: United States
Start Date: August 7, 1995
End Date: August 9, 1995
Accession Number
97N13108
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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