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A mathematical model for Vertical Attitude Takeoff and Landing (VATOL) aircraft simulation. Volume 2: Model equations and base aircraft dataEquations incorporated in a VATOL six degree of freedom off-line digital simulation program and data for the Vought SF-121 VATOL aircraft concept which served as the baseline for the development of this program are presented. The equations and data are intended to facilitate the development of a piloted VATOL simulation. The equation presentation format is to state the equations which define a particular model segment. Listings of constants required to quantify the model segment, input variables required to exercise the model segment, and output variables required by other model segments are included. In several instances a series of input or output variables are followed by a section number in parentheses which identifies the model segment of origination or termination of those variables.
Document ID
19810019547
Acquisition Source
Legacy CDMS
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-2
Report Number: NASA-CR-166129-VOL-2
Accession Number
81N28085
Funding Number(s)
CONTRACT_GRANT: NAS2-10294
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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