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
Aufsatz (Konferenz)
Keine Angabe
Englisch
Aircraft landing buffer device, aircraft landing control system and aircraft
Europäisches Patentamt | 2024
|Aircraft landing control system
NTRS | 1982
|LANDING FACILITY, AIRCRAFT SYSTEM, AND LANDING CONTROL METHOD
Europäisches Patentamt | 2021
|