Sliding mode control for a quadrotor UAV transporting a cable-suspended payload
Özet
In this study, a second-order sliding mode control (2-SMC) strategy has been developed to control a small quadrotor UAV with a suspended payload. It is shown that the existence of a load will cause an oscillation on the system and its movement will remarkably change the dynamics of the quadrotor. In order to overcome this, an upgraded 2-SMC has been suggested to ensure the stability of the system. Firstly, the mathematical model of the quadrotor-suspended payload system is derived based on Lagrange approach, then the suggested controller is designed, and the stability of the system is proved by Lyapunov theory. Finally, numerical simulations are carried out to demonstrate the robustness of the proposed method.
Anahtar Kelimeler
RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/11509Resmi atıflarda kullanılan kalıcı adresAtıflar
- Scopus
- 3
- OpenAlex
- 4
Tam Kayıt
| Alan | Değer | Dil |
|---|---|---|
| dc.contributor.author | Bingöl, Özhan | |
| dc.contributor.author | Güzey, Haci Mehmet | |
| dc.contributor.editor | Ronzhin, A. | |
| dc.contributor.editor | Shishlakov, V. | |
| dc.date.accessioned | 2026-10-22T10:19:05.499858373Z | |
| dc.date.available | 2026-10-22T10:19:05.499858373Z | |
| dc.date.issued | 2020 | |
| dc.description.abstract | In this study, a second-order sliding mode control (2-SMC) strategy has been developed to control a small quadrotor UAV with a suspended payload. It is shown that the existence of a load will cause an oscillation on the system and its movement will remarkably change the dynamics of the quadrotor. In order to overcome this, an upgraded 2-SMC has been suggested to ensure the stability of the system. Firstly, the mathematical model of the quadrotor-suspended payload system is derived based on Lagrange approach, then the suggested controller is designed, and the stability of the system is proved by Lyapunov theory. Finally, numerical simulations are carried out to demonstrate the robustness of the proposed method. | |
| dc.identifier.doi | 10.1007/978-981-13-9267-2_24 | |
| dc.identifier.endpage | 303 | |
| dc.identifier.isbn | 978-981139266-5 | |
| dc.identifier.issn | 2190-3018 | |
| dc.identifier.scopus | 2-s2.0-85072888018 | |
| dc.identifier.startpage | 289 | |
| dc.identifier.uri | https://rdlopen.rawdatalibrary.net/r/gumushane/11509 | |
| dc.identifier.volume | 154 | |
| dc.language.iso | en | |
| dc.publisher | Springer Science and Business Media Deutschland GmbH | |
| dc.relation.conference | 14th International Conference on Electromechanics and Robotics - Zavalishin's Readings, ER(ZR) 2019 | |
| dc.relation.ispartof | Smart Innovation, Systems and Technologies | |
| dc.rights | info:eu-repo/semantics/closedAccess | |
| dc.subject | Quadrotor control | |
| dc.subject | Quadrotor transporting payload | |
| dc.subject | Sliding mode control | |
| dc.subject.other | Aircraft control | |
| dc.subject.other | Numerical methods | |
| dc.subject.other | Robotics | |
| dc.subject.other | System stability | |
| dc.subject.other | Unmanned aerial vehicles (UAV) | |
| dc.subject.other | Lagrange approach | |
| dc.subject.other | Lyapunov theories | |
| dc.subject.other | Payload systems | |
| dc.subject.other | Quad rotors | |
| dc.subject.other | Quad-rotor UAV | |
| dc.subject.other | Quadrotor controls | |
| dc.subject.other | Second-order sliding-mode control | |
| dc.subject.other | Sliding mode control | |
| dc.title | Sliding mode control for a quadrotor UAV transporting a cable-suspended payload | |
| dc.type | Conference Object | |
| dspace.entity.type | Publication | |
| rdl.citation.openalex | 4 | |
| rdl.citation.scopus | 3 | |
| rdl.conference.date | 17 April 2019 through 20 April 2019 | |
| rdl.conference.place | Kursk | |
| rdl.oa.status | closed | |
| rdl.scopus.quartile | Q4 | |
| rdl.source.index | SCOPUS |
