This paper presents the results of attitude, velocity, heave and yaw controller design for an autonomous model scaled helicopter using identified model of vehicle dynamic from parameterized state-space model with quasi-steady attitude dynamic approximation (6 Degree of Freedom model). Multivariable state-space control methodology such as pole placement was used to design the linear state-space feedback for the stabilization of helicopter because of its simple controller architecture. The design specification for controller design was selected according to Military Handling Qualities Specification ADS-33C. Results indicate that acceptable controller can be designed using pole placement method with quasi-steady attitude approximation and it has been shown that the controller design was compliance with design criteria of hover requirement in ADS-33C.
The Effectiveness of Pole Placement Method in Control System Design for an Autonomous Helicopter Model in Hovering Flight
2009-12-30
International Journal of Integrated Engineering; Vol 1 No 3 (2009) ; 2600-7916 ; 2229-838X
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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