On the Synthesis of a Linear Quadratic Controller for a Quadcopter

Hendra Gunawan Harno(1*),

(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.

Full Text:

PDF


DOI: https://doi.org/10.24071/ijasst.v1i2.1919

Refbacks

  • There are currently no refbacks.









Publisher : Faculty of Science and Technology

Society/Institution : Sanata Dharma University

 

 

 

Creative Commons License
This work is licensed under a Creative Commons Attribution 4.0 International License.