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Development and validation of a general purpose linearization program for rigid aircraft modelsThis paper discusses a FORTRAN program that provides the user with a powerful and flexible tool for the linearization of aircraft models. The program LINEAR numerically determines a linear systems model using nonlinear equations of motion and a user-supplied, nonlinear aerodynamic model. The system model determined by LINEAR consists of matrices for both the state and observation equations. The program has been designed to allow easy selection and definition of the state, control, and observation variables to be used in a particular model. Also, included in the report is a comparison of linear and nonlinear models for a high-performance aircraft.
Document ID
19850063825
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Duke, E. L.
(NASA Flight Research Center Edwards, CA, United States)
Antoniewicz, R. F.
(NASA Flight Research Center Edwards, CA, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 85-1891
Accession Number
85A45976
Distribution Limits
Public
Copyright
Other

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