Combined Quadrotor Autopilot System and Differential Morphing System Design
Abstract
The aim of this article is to design and model a quadrotor with autopilot system and differential morphing using the Simultaneous Perturbation Stochastic Approximation (SPSA) optimization algorithm. Along with differential morphing, quadrotor modelling and control was also done. Although it is simple in structure, it has a complex structure in terms of model and control. Newton-Euler method was used for the dynamic model. Non-linear motion equations have been converted to linear motion equations. The full quadrotor model was drawn in the Solidworks program. Mass and moment of inertia information was obtained from this model. Simulation model was created by using state space model approach in Matlab / Simulink environment. Proportional integral derivative (PID) algorithm was used as the control structure. Differential morphing and PID coefficients rates were determined with SPSA. With the optimization method, determining the differential morphing rate, PID coefficients and applying it to the quadrotor provides a very innovative method.
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References
- T. Oktay and O. Kose, “Dynamic Modeling and Control Research Based Quadcopter,” in 2nd International Congress on Multidisciplinary Studies, 2018, pp. 1–17, [Online]. Available: https://kongre.akademikiletisim.com/files/multi2018/Muhendislik_ve_Fen_Bilimleri.pdf.
- O. Kose and T. Oktay, “Optimal Tunning of PID Controller For Forward Flight of Research Based Quadrotor,” 2. Uluslararası Multidisipliner Çalışmaları Kongresi. Adana, 2018.
- A. Mulyadi and B. Siswojo, “Modeling and Control Design of Quadcopter Motor,” vol. 2, no. 2, pp. 34–45, 2020.
- B. Milan, M. V. Toskić, M. Bodić, and V. Rajs, “Advantages of a combination of PD and PID controller over PID controller in the example of quadcopter control and stabilization,” vol. 4, no. 1, pp. 43–50, 2020, doi: 10.7251/IJEEC2001043B.
- D. A. Wallace, “Dynamics and control of a quadrotor with active geometric morphing,” 2016.
- N. Bucki and M. W. Mueller, “Design and Control of a Passively Morphing quadcopter,” in 2019 International Conference on Robotics and Automation (ICRA), 2019, pp. 9116–9122.
- G. Barbaraci, “Modeling and control of a quadrotor with variable geometry arms,” J. Unmanned Veh. Syst., vol. 3, no. 2, pp. 35–57, 2015.
- T. Oktay and O. Kose, “The Effect of Collective Morphing on the Lateral Flight in Quadcopter,” Umteb6. UluslararasiMesleki ve Teknik Bilimler Kongresi. Iğdır, 2019.
Details
Primary Language
English
Subjects
Aerospace Engineering
Journal Section
Research Article
Publication Date
December 20, 2021
Submission Date
January 8, 2021
Acceptance Date
July 30, 2021
Published in Issue
Year 2021 Volume: 5 Number: 2
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