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Quasi-optimum design of an aircraft landing control system.Quasi-optimum control law for aircraft landing control system design based on Friedland technique, evaluating effectiveness by computer simulation
Document ID
19690065291
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ling, C. K.
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
69A43280
Funding Number(s)
CONTRACT_GRANT: NAS2-3636
Distribution Limits
Public
Copyright
Other

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