On the Synthesis of a Linear Quadratic Controller for a Quadcopter
(1) Department of Aerospace and Software Engineering Gyeongsang National University Republic of Korea
(*) Corresponding Author
Abstract
This paper discusses about synthesizing a state-feedback controller for a quadcopter based on an optimal linear quadratic control method. The resulting flight control system enables the quadcopter to maintain stability and to track a reference input. The solution to this control problem involves solving an algebraic Riccati equation. The reference-input tracking capability is simulated to show the capability of the quadcopter flight control system.
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PDFDOI: https://doi.org/10.24071/ijasst.v1i2.1919
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Publisher : Faculty of Science and Technology
Society/Institution : Sanata Dharma University
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