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Computing Linear Mathematical Models Of AircraftDerivation and Definition of Linear Aircraft Model (LINEAR) computer program provides user with powerful, and flexible, standard, documented, and verified software tool for linearization of mathematical models of aerodynamics of aircraft. Intended for use in software tool to drive linear analysis of stability and design of control laws for aircraft. Capable of both extracting such linearized engine effects as net thrust, torque, and gyroscopic effects, and including these effects in linear model of system. Designed to provide easy selection of state, control, and observation variables used in particular model. Also provides flexibility of allowing alternate formulations of both state and observation equations. Written in FORTRAN.
Document ID
19910000099
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Duke, Eugene L.
(NASA Ames Research Center, Moffett Field, CA.)
Antoniewicz, Robert F.
(NASA Ames Research Center, Moffett Field, CA.)
Krambeer, Keith D.
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ARC-12422
Accession Number
91B10099
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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