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Application of quadratic optimization to helicopter flight control.Quadratic optimization applied to helicopter flight control design, assuming constant feedback gains and command step input with zero steady state error
Document ID
19690065290
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gray, D. L.
Rempfer, P. S.
Stevenson, L.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Publication Information
Publisher: AMERICAN INST. OF CHEMICAL ENGINEERS,
Subject Category
Aircraft
Meeting Information
Meeting: AMERICAN AUTOMATIC CONTROL COUNCIL, JOINT AUTOMATIC CONTROL CONFERENCE
Location: BOULDER, COLO.
Start Date: August 5, 1969
End Date: August 7, 1969
Sponsors: AMERICAN AUTOMATIC CONTROL COUNCIL
Accession Number
69A43279
Distribution Limits
Public
Copyright
Other

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