College - Author 1
College of Engineering
Department - Author 1
Aerospace Engineering Department
College - Author 2
College of Engineering
Department - Author 2
Aerospace Engineering Department
College - Author 3
College of Engineering
Department - Author 3
Aerospace Engineering Department
College - Author 4
College of Engineering
Department - Author 4
Aerospace Engineering Department
Advisor
Chokri Sendi, College of Engineering, Aerospace Engineering Department
Funding Source
Metrea
Acknowledgements
California Polytechnic State University
Date
10-2024
Abstract/Summary
This project revolves around creating an a attitude controller for a hovering flexible flapping wing UAV that is based on a flying hummingbird. We based our model from a paper by Banazadeh and Taymourtash1 , First replicating the open-loop results using the nonlinear dynamic model and the equations of motion (seen below) while considering aerodynamic loads. Once replicated, we then used fuzzy logic to model the dynamic model. Subsequently, we designed a fuzzy controller to stabilize the hovering mode. We then considered and detailed future work needed to make further progress in this area.
October 1, 2024.
URL: https://digitalcommons.calpoly.edu/ceng_surp/57