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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 ...
PID controlling of the Quadrotor and sensor performance tests
(World Scientific and Engineering Academy and Society, 2014)
This paper includes three main parts. The first part is about a Quadrotor as a type of unmanned vehicles. The second part includes its mathematical model and controlling with PID controller. The last part consists of some ...