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    ARTICLE

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

    Ivan Paulo Canal1,*, Manuel Martin Pérez Reimbold2, Maurício de Campos2

    CMES-Computer Modeling in Engineering & Sciences, Vol.125, No.1, pp. 65-75, 2020, DOI:10.32604/cmes.2020.010741 - 18 September 2020

    Abstract An aircraft quadrotor is a complex control system that allows for great flexibility in flight. 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 of the aircraft, making it necessary to adapt the control system for this situation. Among the various control methods that have been investigated, proportional-integralderivative (PID) control offers good results and simplicity of application; however, achieving stability and high performance is challenging, with the most critical task being tuning the controller gains. The… More >

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