Optimal Flight Control System Design Using LQR: A Study on Load Minimum and Drift Minimum Analysis
International Journal of Science and Research (IJSR)

International Journal of Science and Research (IJSR)
Call for Papers | Fully Refereed | Open Access | Double Blind Peer Reviewed

ISSN: 2319-7064


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Informative Article | Science and Technology | India | Volume 10 Issue 6, June 2021 | Popularity: 5.1 / 10


     

Optimal Flight Control System Design Using LQR: A Study on Load Minimum and Drift Minimum Analysis

Ramona Devi


Abstract: This paper outlines the core principles underlying flight control, including both analysis and design aspects. The Linear Quadratic Regulator (LQR) control methodology is employed to attain performance, stability, and robustness. It delves into essential concepts such as load minimization and drift minimization. The control system's design is subsequently simulated and subjected to analysis using Simulink.


Keywords: optimal, LQR, flight, control, autopilot


Edition: Volume 10 Issue 6, June 2021


Pages: 1789 - 1792


DOI: https://www.doi.org/10.21275/SR231208203343


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Ramona Devi, "Optimal Flight Control System Design Using LQR: A Study on Load Minimum and Drift Minimum Analysis", International Journal of Science and Research (IJSR), Volume 10 Issue 6, June 2021, pp. 1789-1792, https://www.ijsr.net/getabstract.php?paperid=SR231208203343, DOI: https://www.doi.org/10.21275/SR231208203343

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