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Continuation Methods for Qualitative Analysis of Aircraft DynamicsA class of numerical methods for constructing bifurcation curves for systems of coupled, non-linear ordinary differential equations is presented. Foundations are discussed, and several variations are outlined along with their respective capabilities. Appropriate background material from dynamical systems theory is presented.
Document ID
20040110969
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Cummings, Peter A.
(National Inst. of Aerospace Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2004
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA/CR-2004-213035
NIA-2004-06
Report Number: NASA/CR-2004-213035
Report Number: NIA-2004-06
Funding Number(s)
OTHER: 23-762-60-31
CONTRACT_GRANT: NCC1-02043
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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