NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Piloted evaluation of an integrated propulsion and flight control simulatorA piloted evaluation of the integrated flight and propulsion control simulator for advanced integrated propulsion and airframe control design is described. The evaluation will cover control effector gains and deadbands, control effectiveness and control authority, and heads up display functionality. For this evaluation the flight simulator is configured for transition flight using an advanced Short Take-Off and Vertical Landing fighter aircraft model, a simplified high-bypass turbofan engine model, fighter cockpit displays, and pilot effectors. The piloted tasks used for rating displays and control effector gains are described. Pilot comments and simulation results confirm that the display symbology and control gains are very adequate for the transition flight task. Additionally, it is demonstrated that this small-scale, fixed base flight simulator facility can adequately perform a real time, piloted control evaluation.
Document ID
19920024863
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bright, Michelle M.
(NASA Lewis Research Center Cleveland, OH, United States)
Simon, Donald L.
(Army Aviation Systems Command Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Aircraft Stability And Control
Report/Patent Number
AD-A254805
NAS 1.15:105797
AVSCOM-TR-92-C-028
E-7227
NASA-TM-105797
Meeting Information
Meeting: Flight Simulation Technologies Conference and Exhibit
Location: Hilton Head, SC
Country: United States
Start Date: August 24, 1992
End Date: August 26, 1992
Sponsors: AIAA
Accession Number
92N34107
Funding Number(s)
PROJECT: RTOP 505-62-50
Distribution Limits
Public
Copyright
Public Use Permitted.
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available