Quasi-optimum control law for aircraft landing control system design based on Friedland technique, evaluating effectiveness by computer simulation
Quasi-optimum design of an aircraft landing control system.
AMERICAN AUTOMATIC CONTROL COUNCIL, JOINT AUTOMATIC CONTROL CONFERENCE ; 1969 ; BOULDER, COLO.
1969-01-01
Conference paper
No indication
English
Aircraft landing control system
NTRS | 1982
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