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A Mathematical Model for Vertical Attitude Takeoff and Landing (VATOL) Aircraft Simulation: Model Description Application - Volume 1A mathematical model of a high performance airplane capable of vertical attitude takeoff and landing (VATOL) was developed. An off line digital simulation program incorporating this model was developed to provide trim conditions and dynamic check runs for the piloted simulation studies and support dynamic analyses of proposed VATOL configuration and flight control concepts. Development details for the various simulation component models and the application of the off line simulation program, Vertical Attitude Take-Off and Landing Simulation (VATLAS), to develop a baseline control system for the Vought SF-121 VATOL airplane concept are described.
Document ID
19810019546
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Fortenbaugh, R. L. (Vought Corp. Dallas, TX, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-166129-VOL-1
Report Number: NASA-CR-166129-VOL-1
Accession Number
81N28084
Funding Number(s)
CONTRACT_GRANT: NAS2-10294
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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