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Generic Airplane Model Concept and Four Specific Models Developed for Use in Piloted Simulation StudiesA generic airplane model concept was developed to allow configurations with various agility, performance, handling qualities, and pilot vehicle interface to be generated rapidly for piloted simulation studies. The simple concept allows stick shaping and various stick command types or modes to drive an airplane with both linear and nonlinear components. Output from the stick shaping goes to linear models or a series of linear models that can represent an entire flight envelope. The generic model also has provisions for control power limitations, a nonlinear feature. Therefore, departures from controlled flight are possible. Note that only loss of control is modeled, the generic airplane does not accurately model post departure phenomenon. The model concept is presented herein, along with four example airplanes. Agility was varied across the four example airplanes without altering specific excess energy or significantly altering handling qualities. A new feedback scheme to provide angle-of-attack cueing to the pilot, while using a pitch rate command system, was implemented and tested.
Document ID
19970017364
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Hoffler, Keith D.
(Vigyan Research Associates, Inc. Hampton, VA United States)
Fears, Scott P.
(Vigyan Research Associates, Inc. Hampton, VA United States)
Carzoo, Susan W.
(Unisys Corp. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1997
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-201651
NAS 1.26:201651
Report Number: NASA-CR-201651
Report Number: NAS 1.26:201651
Accession Number
97N19656
Funding Number(s)
CONTRACT_GRANT: NAS1-96014
CONTRACT_GRANT: NAS1-20454
CONTRACT_GRANT: NAS1-19672
PROJECT: RTOP 505-68-30-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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