In this study, an experimental set of a Single-DOF Copter system is created and transfer functions that could model the dynamics of the physical system with high accuracy were investigated. In order to model the dynamics of the physical system with the highest accuracy, five different transfer functions have been proposed, in which the zero and pole values are determined by optimizing with the Vibrating Particle System Algorithm. ISE, ITAE, IAE, ITSE functions, which are widely used in the literature in determining transfer functions, are determined as objective functions. In order to verify the transfer functions, the responses of the transfer functions and the experimental system response are presented comparatively, and their suitability was evaluated. It has been observed that the proposed method is successful in defining the transfer function of the experimental system, and the compatibility of the obtained transfer functions with the system response is between 75.407% and 98.612% accuracy.
VPSA system identificaiton transfer function single-dof copter optimisation
Birincil Dil | İngilizce |
---|---|
Konular | Makine Mühendisliği (Diğer), Uçak Performansı ve Uçuş Kontrol Sistemleri, Uçuş Dinamiği |
Bölüm | Research Articles |
Yazarlar | |
Yayımlanma Tarihi | 30 Aralık 2023 |
Gönderilme Tarihi | 28 Eylül 2023 |
Yayımlandığı Sayı | Yıl 2023 Cilt: 04 Sayı: 02 |
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