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Nonlinear transformatA technique for designing automatic flight controllers for aircraft which utilizes the transformation theory of nonlinear systems to linear systems is presently being developed at NASA Ames Research Center. A method is considered in which a given nonlinear is transformed to a controllable linear system in Brunovsky canonical form. A linear approximation is introduced to the nonlinear system called the modified tangent model. This model is easily computed. Constructing the transformation for this model enables the designer to find an approximate transformation for the nonlinear system.
Document ID
19840007809
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ford, H.
(Texas Technological Univ. Lubbock, TX, United States)
Hunt, L. R.
(Texas Technological Univ. Lubbock, TX, United States)
Su, R.
(Texas Technological Univ. Lubbock, TX, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Systems Analysis
Report/Patent Number
NAS 1.26:166506
NASA-CR-166506
Report Number: NAS 1.26:166506
Report Number: NASA-CR-166506
Accession Number
84N15877
Funding Number(s)
CONTRACT_GRANT: NAG2-189
CONTRACT_GRANT: NAG2-203
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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