The paper is devoted to the mathematical modelling and construction of various control laws for a quadcopter. Mathematical model of quadcopter is considered. One of the approachesfor controllerconstruction is the proportionalintegral–derivative controller, which is simple in comparison with other methods. Another approach is the linear quadratic regulator, that has good performance. The results of construction of the controllers and modelling the closed-loop systems are presented.
Key words: stabilization, control, quadcopter
Topic: ENGINEERING SCIENCES