NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of asymmetrical nonlinear oscillations in the parameter plane.Parameter-plane method analysis of nonlinear equations of asymmetric oscillations in adaptive feedback control systems
Document ID
19660057450
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Siljak, D. D.
Date Acquired
August 3, 2013
Publication Date
April 1, 1966
Publication Information
Publication: IEEE TRANSACTIONS ON AUTOMATIC "ONTROL
Subject Category
Electronics
Accession Number
66A36740
Funding Number(s)
CONTRACT_GRANT: NAS2-2609
Distribution Limits
Public
Copyright
Other
Keywords
FEEDBACK CONTROL SYSTEM
NONLINEAR EQUATION
ADAPTIVE CONTROL
FORCED OSCILLATION

Available Downloads

There are no available downloads for this record.
No Preview Available