Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis
American Journal of Astronomy and Astrophysics
Volume 8, Issue 2, June 2020, Pages: 15-18
Received: Oct. 20, 2019;
Accepted: Apr. 7, 2020;
Published: Apr. 17, 2020
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Thanda Win, Department of Electronic Engineering, West Yangon Technological University, Yangon Region, Republic of the Union of Myanmar
Hteik Tin Cho Nyunt, Department of Electronic Engineering, Government Technical High School (Shwe Pyi Thar), Yangon Region, Republic of the Union of Myanmar
Hla Myo Tun, Department of Electronic Engineering, Yangon Technological University, Yangon Region, Republic of the Union of Myanmar
The paper presents the analysis on stability of digital control system for unmanned vehicle with numerical analysis. The objective of this study is mainly emphasized on the fulfillment of the advanced control techniques according to the fundamental concepts of digital control system approaches for unmanned aerial vehicle system design. The targeted unmanned aerial vehicle system was designed based on the simple construction under the idea of fixed wing flight system approaches. The stability analyses on unmanned aerial vehicle are vital role to enhance the real world applications. The background concepts on digital control system for stability analysis on dynamic control system like unmanned aerial vehicle system. The appropriate controller design for dynamic control system of unmanned aerial vehicle is vital role to analyze the accurate stability condition for reality. The implementation of numerical analysis on compensator design has been developed by using MATLAB. The physical parameters in these analyses are based on the experimental outcomes from the recent research works in dynamical system implementations. The mathematical approaches are very helpful for numerical analysis on compensator design for the unmanned aerial vehicles schemes. The simulation results confirm that the high performance stability test on unmanned aerial vehicle system has been met with the theoretical works.
Hteik Tin Cho Nyunt,
Hla Myo Tun,
Stability of Digital Control System for Unmanned Aerial Vehicle with Numerical Analysis, American Journal of Astronomy and Astrophysics.
Vol. 8, No. 2,
2020, pp. 15-18.
Copyright © 2020 Authors retain the copyright of this article.
This article is an open access article distributed under the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/
) which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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