Downloads: 2 | Views: 256 | Weekly Hits: ⮙1 | Monthly Hits: ⮙1
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
Please Disable the Pop-Up Blocker of Web Browser
Verification Code will appear in 2 Seconds ... Wait