Ziegler-Nichols Customization for Quadrotor Attitude Control under Empty and Full Loading Conditions

An aircraft quadrotor is a complex control system that allows for great flexibility inflight. Controlling multirotor aerial systems such as quadrotors is complex because the variables involved are not always available, known, and accurate. The inclusion of payload changes the dynamic characteristics...

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Veröffentlicht in:	Computer modeling in engineering & sciences 2020-01, Vol.125 (1), p.65-75
Hauptverfasser:	Canal, Ivan Paulo, Reimbold, Manuel Martin Pérez, de Campos, Maurício
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Attitude control Complex variables Control methods Control stability Control systems Controllers Dynamic characteristics Mathematical analysis Multirotor Pid Tuning Pitch (inclination) Proportional integral derivative Quadrotor Control Rolling motion Rotary wing aircraft Tuning Ziegler-Nichols
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