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• W2949357810 startingPage "02001" @default.
• W2949357810 abstract "This paper aim is to present a comparative study between Linear Quadratic Regulator (LQR), Linear Quadratic Gaussian (LQG) and nonlinear controllers for pitch control of a fixed-wing Unmanned Aerial Vehicle (UAV). Due to a good stability margin and strong robustness LQR has been selected. LQG was chosen because is able to overcome external disturbances. Kalman Filter controller was also introduced to the fixed-wing UAV flight control. Further, we designed an autopilot that controls the pitch angle of the fixed-wing UAV. In the end, the control laws are simulated in Matlab/Simulink. The results obtained are compared to see which method is faster, more reliable and more robust." @default.
• W2949357810 created "2019-06-27" @default.
• W2949357810 creator A5011709334 @default.
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• W2949357810 date "2019-01-01" @default.
• W2949357810 modified "2023-09-27" @default.
• W2949357810 title "Control of longitudinal flight dynamics of a fixedwing UAV using LQR, LQG and nonlinear control" @default.
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• W2949357810 doi "https://doi.org/10.1051/e3sconf/201910402001" @default.
• W2949357810 hasPublicationYear "2019" @default.
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