NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Flight Tests of a Ministick Controller in an F/A-18 AirplaneIn March of 1999, five pilots performed flight tests to evaluate the handling qualities of an F/A-18 research airplane equipped with a small-displacement center stick (ministick) controller that had been developed for the JAS 39 Gripen airplane (a fighter/attack/ reconnaissance airplane used by the Swedish air force). For these tests, the ministick was installed in the aft cockpit (see figure) and production support flight control computers (PSFCCs) were used as interfaces between the controller hardware and the standard F/A-18 flight-control laws. The primary objective of the flight tests was to assess any changes in handling qualities of the F/A-18 airplane attributable to the mechanical characteristics of the ministick. The secondary objective was to demonstrate the capability of the PSFCCs to support flight-test experiments.
Document ID
20110023811
Acquisition Source
Armstrong Flight Research Center
Document Type
Other - NASA Tech Brief
Authors
Stoliker, Patrick C.
(NASA Dryden Flight Research Center Edwards, CA, United States)
Carter, John
(NASA Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2003
Publication Information
Publication: NASA Tech Briefs, May 2003
Subject Category
Aircraft Stability And Control
Report/Patent Number
DRC-01-33
Distribution Limits
Public
Copyright
Public Use Permitted.
No Preview Available