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
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 Ziegler–Nichols (ZN) theory
was used… More >
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