Fault tolerant control of a quadrotor based on incremental nonlinear dynamic inversion
dc.authorid | 0000-0002-2066-6016 | en_US |
dc.authorid | 0000-0002-2633-3351 | en_US |
dc.authorid | 0000-0003-1836-2600 | en_US |
dc.contributor.author | Ahmadi, Karim | |
dc.contributor.author | Asadi, Davood | |
dc.contributor.author | Nabavi-Chashmi, Seyed-Yaser | |
dc.date.accessioned | 2022-08-25T12:14:55Z | |
dc.date.available | 2022-08-25T12:14:55Z | |
dc.date.issued | 30.04.2022 | en_US |
dc.department | Başka Kurum | en_US |
dc.description.abstract | The multirotor unmanned aerial vehicles (UAVs) have rapidly attracted interest of the researchers since they play a unique role in a variety of areas including the military, agriculture, rescue, and mining. Actuator fault or failure is inevitable during multi-rotor’s operations, which can endanger humans on the ground in addition to costly damage to the system itself. Therefore, this paper introduces a nonlinear controller algorithm for fault-tolerant control of a quadcopter with partial loss of actuator effectiveness. The introduced controller includes a cascade structure of the fast inner-loop dynamics and slow outer-loop dynamics. In the inner-loop part of the controller, an incremental nonlinear dynamic inversion controller is applied and a modified PID control algorithm is used in the outer-loop of the controller. Simulation results for different fault scenarios demonstrate that the proposed fault-tolerant controller approach can quickly adapt itself to the abrupt change due to the motor faults and tracks the desired inputs satisfactorily. | en_US |
dc.identifier.citation | Ahmadi, K., Asadi, D., Nabavi-Chashmi, S. Y. (2022). Fault tolerant control of a quadrotor based on incremental nonlinear dynamic inversion. International Journal of Aeronautics and Astronautics, 3, (1), 28-47. | en_US |
dc.identifier.endpage | 47 | en_US |
dc.identifier.issn | 2757-6574 | en_US |
dc.identifier.issue | 1 | en_US |
dc.identifier.startpage | 28 | en_US |
dc.identifier.uri | https://hdl.handle.net/20.500.12395/43003 | |
dc.identifier.volume | 3 | en_US |
dc.language.iso | en | en_US |
dc.publisher | Selçuk Üniversitesi | en_US |
dc.relation.ispartof | International Journal of Aeronautics and Astronautics | en_US |
dc.relation.publicationcategory | Makale - Uluslararası Hakemli Dergi - Başka Kurum Yazarı | en_US |
dc.rights | info:eu-repo/semantics/openAccess | en_US |
dc.selcuk | 20240510_oaig | en_US |
dc.subject | Fault Tolerant Control | en_US |
dc.subject | Hata Toleranslı Kontrol | en_US |
dc.subject | Çok Rotorlu | en_US |
dc.subject | Doğrusal Olmayan Dinamik Ters Çevirme | en_US |
dc.subject | Multirotor | en_US |
dc.subject | Nonlinear Dynamic Inversion | en_US |
dc.subject | Incremental | en_US |
dc.subject | Artımlı | en_US |
dc.title | Fault tolerant control of a quadrotor based on incremental nonlinear dynamic inversion | en_US |
dc.type | Article | en_US |