Araştırma Makalesi
Yıl 2023,
Cilt: 8 Sayı: 2, 28 - 39, 31.12.2023
Öz
Kaynakça
- [1] SpaceX, “FALCON User's Guide,” SpaceX, 2021.
- [2] R. Ferrante, A roboust control approach for rocket landing, Edinburgh: University of Edinburgh, 2017.
- [3] G. Z. Prous, Guidance and Control for Launch and Vertical Descend of Resuable Launchers using Model Predictive Control and Convex Optimization, Sweden: Luleå University of Technology, 2020.
- [4] G. M. Siouris, Missile Guidance and Control Systems, USA: Springer-Verlag New York, Inc., 2004.
- [5] O. B. G. P. Sutton, Rocket Propulsion Elements, Hoboken: New Jersey: John Wiley & Sons, Inc, 2017. , 2017.
- [6] A. A. Martin, Model Predictive Control for Ascent Load Management of a Reusable Launch Vehicle, Massachusetts Institute of Technology, 2022.
- [7] O. Acar, İ. Göv, M. H. Doğru, Comparison of Open Source and Hardware Flight Controllers, The international Conference of materials and Engineering Technology, 234-246, 2019.
- [8] B. Çiftcioğlu, İ. Göv, M. H. Doğru, Static Structural Analysis of a Rc Helicopter Tailrotor, The international Conference of materials and Engineering Technology, 927-938, 2019.
- [9] J. H. Blakelock, Automatic control of aircraft and missiles, Wiley, 1965.
- [10] T. W. M. R. W. Beard, Small Unmanned Aircraft Theory and Practice, New Jersey 08540: Princeton University Press, 2012.
- [11] F. L. L. E. N. J. Brian L. Stevens, Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, John Wiley & Sons, 2015.
- [12] C. A. Osheku, Ballistics, IntechOpen, 2019.
- [13] G. M. Siouris, Missile Guidance and Control Systems, Springer Science & Business Media, 2004.
- [14] S. B. A. B. Carlo Alberto Pascucci, Model Predictive Control for Powered Descent Guidance and Control, 2015 European Control Conference, 2015.
- [15] C. B. A. Eduardo F. Camacho, Model Predictive Control, Springer, 2004.
COMPARATIVE STUDY OF PID AND MPC CONTROLLERS FOR VERTICAL TAKE-OFF AND VERTICAL LANDING (VTVL) ROCKET CONTROL
Öz
This study delves into the intricacies of designing a controller for the creation of a simulation environment dedicated to rocket flight and vertical landing. The primary focus is on evaluating two prominent control mechanisms: the Proportional-Integral-Derivative (PID) controller and the Model Predictive Control (MPC) controller. The study systematically explores the performance of these controllers in the context of vertical descent, revealing that the PID controller effectively enhances the rocket's vertical descent capabilities. Additionally, the research underscores the MPC controller's remarkable potential in augmenting vertical descent performance through the adept coordination of various control mechanisms and its ability to adapt to external disturbances. The findings of this study not only contribute significantly to the field of rocket control but also establish a foundational framework for future endeavours and advancements in this dynamic and crucial domain.
Anahtar Kelimeler
Kaynakça
- [1] SpaceX, “FALCON User's Guide,” SpaceX, 2021.
- [2] R. Ferrante, A roboust control approach for rocket landing, Edinburgh: University of Edinburgh, 2017.
- [3] G. Z. Prous, Guidance and Control for Launch and Vertical Descend of Resuable Launchers using Model Predictive Control and Convex Optimization, Sweden: Luleå University of Technology, 2020.
- [4] G. M. Siouris, Missile Guidance and Control Systems, USA: Springer-Verlag New York, Inc., 2004.
- [5] O. B. G. P. Sutton, Rocket Propulsion Elements, Hoboken: New Jersey: John Wiley & Sons, Inc, 2017. , 2017.
- [6] A. A. Martin, Model Predictive Control for Ascent Load Management of a Reusable Launch Vehicle, Massachusetts Institute of Technology, 2022.
- [7] O. Acar, İ. Göv, M. H. Doğru, Comparison of Open Source and Hardware Flight Controllers, The international Conference of materials and Engineering Technology, 234-246, 2019.
- [8] B. Çiftcioğlu, İ. Göv, M. H. Doğru, Static Structural Analysis of a Rc Helicopter Tailrotor, The international Conference of materials and Engineering Technology, 927-938, 2019.
- [9] J. H. Blakelock, Automatic control of aircraft and missiles, Wiley, 1965.
- [10] T. W. M. R. W. Beard, Small Unmanned Aircraft Theory and Practice, New Jersey 08540: Princeton University Press, 2012.
- [11] F. L. L. E. N. J. Brian L. Stevens, Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, John Wiley & Sons, 2015.
- [12] C. A. Osheku, Ballistics, IntechOpen, 2019.
- [13] G. M. Siouris, Missile Guidance and Control Systems, Springer Science & Business Media, 2004.
- [14] S. B. A. B. Carlo Alberto Pascucci, Model Predictive Control for Powered Descent Guidance and Control, 2015 European Control Conference, 2015.
- [15] C. B. A. Eduardo F. Camacho, Model Predictive Control, Springer, 2004.
Toplam 15 adet kaynakça vardır.
Ayrıntılar
| Birincil Dil | İngilizce |
|---|---|
| Konular | Makine Teorisi ve Dinamiği |
| Bölüm | Research Article |
| Yazarlar | |
| Yayımlanma Tarihi | 31 Aralık 2023 |
| Gönderilme Tarihi | 18 Kasım 2023 |
| Kabul Tarihi | 4 Aralık 2023 |
| Yayımlandığı Sayı | Yıl 2023 Cilt: 8 Sayı: 2 |
IMPORTANT NOTES
No part of the material protected by this copyright may be reproduced or utilized in any form or by any means, without the prior written permission of the copyright owners, unless the use is a fair dealing for the purpose of private study, research or review. The authors reserve the right that their material can be used for purely educational and research purposes. All the authors are responsible for the originality and plagiarism, multiple publication, disclosure and conflicts of interest and fundamental errors in the published works.
*Please note that All the authors are responsible for the originality and plagiarism, multiple publication, disclosure and conflicts of interest and fundamental errors in the published works. Author(s) submitting a manuscript for publication in IJEES also accept that the manuscript may go through screening for plagiarism check using IThenticate software. For experimental works involving animals, approvals from relevant ethics committee should have been obtained beforehand assuring that the experiment was conducted according to relevant national or international guidelines on care and use of laboratory animals. Authors may be requested to provide evidence to this end.
**Authors are highly recommended to obey the IJEES policies regarding copyrights/Licensing and ethics before submitting their manuscripts.
Copyright © 2023. AA. All rights reserved