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Toplam kayıt 6, listelenen: 1-6
Performance comparison of yaw rate damping controllers
(2013)
Maintaining desired flight conditions in flight envelope for a long period is one of the primary control problems in aircraft flight control. Aircraft dynamics are in general nonlinear, time varying and uncertain. A control ...
Pitch rate damping of an aircraft by a fuzzy PD controller
(2010)
Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics ...
Pitch rate damping of an aircraft by fuzzy and classical PD controller
(2010)
Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics ...
Comparison of classical PD and fuzzy PD controller performances of an aircraft pitch angle control system
(2011)
Aircraft dynamics are in general nonlinear, time varying, and uncertain. A control system (classical control systems) designed for a flight condition, may not provide the desired stability and performance characteristics ...
ARINC 629 data bus standard on aircrafts
(2010)
In earlier analogue avionic systems the number of cables used to transfer information between the various system components was considerable. With these systems, at least one pair of wires has been required for each signal ...
Training of the maintenance personnel to prevent failures in aircraft systems
(Pergamon-Elsevier Science LTD, 2011)
The aircraft maintenance process plays a vital role in aviation safety. The quality of the maintenance process and the qualifications of the aircraft maintenance personnel are important factors in the safety of aircraft. ...