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