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Flight simulation software at NASA Dryden Flight Research CenterThe NASA Dryden Flight Research Center has developed a versatile simulation software package that is applicable to a broad range of fixed-wing aircraft. This package has evolved in support of a variety of flight research programs. The structure is designed to be flexible enough for use in batch-mode, real-time pilot-in-the-loop, and flight hardware-in-the-loop simulation. Current simulations operate on UNIX-based platforms and are coded with a FORTRAN shell and C support routines. This paper discusses the features of the simulation software design and some basic model development techniques. The key capabilities that have been included in the simulation are described. The NASA Dryden simulation software is in use at other NASA centers, within industry, and at several universities. The straightforward but flexible design of this well-validated package makes it especially useful in an engineering environment.
Document ID
19960001686
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Norlin, Ken A.
(NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1995
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-2052
NAS 1.15:104315
NASA-TM-104315
Report Number: H-2052
Report Number: NAS 1.15:104315
Report Number: NASA-TM-104315
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics Flight Simulation Technologies Conference
Location: Baltimore, MD
Country: United States
Start Date: August 7, 1995
End Date: August 10, 1995
Accession Number
96N11694
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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