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Developing a workstation-based, real-time simulation for rapid handling qualities evaluations during designThis paper describes the Rapid Aircraft DynamIcs AssessmeNt (RADIAN) project - an integration of the Aircraft SYNThesis (ACSTNT) design code with the USAD DATCOM code that estimates stability derivatives. Both of these codes are available to universities. These programs are then linked to flight simulation and flight controller synthesis tools and resulting design is evaluated on a graphics workstation. The entire process reduces the preliminary design time by an order of magnitude and provides an initial handling qualities evaluation of the design coupled to a control law. The integrated design process is applicable to both conventional aircraft taken from current textbooks and to unconventional designs emphasizing agility and propulsive control of attitude. The interactive and concurrent nature of the design process has been well received by industry and by design engineers at NASA. The process is being implemented into the design curriculum and is being used by students who view it as a significant advance over prior methods.
Document ID
19950023914
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Anderson, Frederick
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Biezad, Daniel J.
(California Polytechnic State Univ. San Luis Obispo, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:198831
NASA-CR-198831
Report Number: NAS 1.26:198831
Report Number: NASA-CR-198831
Accession Number
95N30335
Funding Number(s)
CONTRACT_GRANT: NCC2-800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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