EN
Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault
Öz
This paper presents a novel nonlinear robust adaptive trajectory tracking control architecture for stabilizing and controlling a quadrotor in the presence of actuator partial faults. The proposed control strategy utilizes an Incremental Nonlinear Dynamic Inversion (INDI) algorithm as the baseline controller in the inner loop and augments a nonlinear model reference adaptive controller in the outer loop to ensure robustness against unmodeled faults. Additionally, a modified PID controller is introduced in the most outer-loop to track the desired path. The effects of actuator faults are modeled by considering sudden variations in motor thrust and torques. To enhance the control algorithm's robustness, a projection operator is employed in the robust adaptive structure. Comparative performance evaluations with a previous successful algorithm implemented on a quadrotor model demonstrate that the proposed controller achieves full controllability of the faulty quadrotor in pitch, roll, and yaw channels in the presence of actuator partial faults up to 50%.
Anahtar Kelimeler
Destekleyen Kurum
Scientific and Technological Research Council of Turkey (TÜBİTAK)
Proje Numarası
120M793
Kaynakça
- [1] Turan V., Avşar E., Asadi D., Aydin E.A., "Image Processing Based Autonomous Landing Zone Detection for a Multi-Rotor Drone in Emergency Situation”, Turkish Journal Engineering 5 (2021): 193-200.
- [2] Asadi D., “Partial engine fault detection and control of a quadrotor considering model uncertainty”, Turkish Journal Engineering 6 (2021):106-117.
- [3] Nabavi Y., Asadi D., Ahmadi K., “Image-based UAV position and velocity estimationsing a monocular camera”, Control Engineering Practice 134 (2023).
- [4] Asadi D., Sabzehparvar M., Atkins E.M., Talebi H.A., “Damaged airplane trajectory planning based on flight envelope and motion primitives”, Journal of Aircraft 51 (2014): 1740-1757.
- [5] Asadi D., Sabzehparvar M., Talebi H.A., “Damaged airplane flight envelope and stability evaluation, Aircraft Engineering and Aerospace Technology”, 85 (2013) : 186-198.
- [6] Ahmadi K., Asadi D., Pazooki F., “Nonlinear L1 adaptive control of an airplane with structural damage”, Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. 233 (2019) : 341-353.
- [7] Asadi D., Ahmadi K., “Nonlinear robust adaptive control of an airplane with structural damage”, Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. 234 (2020) : 2076-2088.
- [8] Asadi D., Bagherzadeh S.A., “Nonlinear adaptive sliding mode tracking control of an airplane with wing damage”, Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. 232 (2017): 1405–1420.
Ayrıntılar
Birincil Dil
İngilizce
Konular
Matematik
Bölüm
Araştırma Makalesi
Erken Görünüm Tarihi
29 Nisan 2024
Yayımlanma Tarihi
30 Nisan 2024
Gönderilme Tarihi
1 Eylül 2022
Kabul Tarihi
28 Ağustos 2023
Yayımlandığı Sayı
Yıl 2024 Cilt: 9 Sayı: 1
APA
Ahmadi Dastgerdi, K., Asadi, D., Nabavi Chashmi, S. Y., & Tutsoy, Ö. (2024). Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault. Journal of Engineering Technology and Applied Sciences, 9(1), 1-21. https://doi.org/10.30931/jetas.1169518
AMA
1.Ahmadi Dastgerdi K, Asadi D, Nabavi Chashmi SY, Tutsoy Ö. Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault. Journal of Engineering Technology and Applied Sciences. 2024;9(1):1-21. doi:10.30931/jetas.1169518
Chicago
Ahmadi Dastgerdi, Karim, Davood Asadi, Seyed Yaser Nabavi Chashmi, ve Önder Tutsoy. 2024. “Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault”. Journal of Engineering Technology and Applied Sciences 9 (1): 1-21. https://doi.org/10.30931/jetas.1169518.
EndNote
Ahmadi Dastgerdi K, Asadi D, Nabavi Chashmi SY, Tutsoy Ö (01 Nisan 2024) Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault. Journal of Engineering Technology and Applied Sciences 9 1 1–21.
IEEE
[1]K. Ahmadi Dastgerdi, D. Asadi, S. Y. Nabavi Chashmi, ve Ö. Tutsoy, “Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault”, Journal of Engineering Technology and Applied Sciences, c. 9, sy 1, ss. 1–21, Nis. 2024, doi: 10.30931/jetas.1169518.
ISNAD
Ahmadi Dastgerdi, Karim - Asadi, Davood - Nabavi Chashmi, Seyed Yaser - Tutsoy, Önder. “Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault”. Journal of Engineering Technology and Applied Sciences 9/1 (01 Nisan 2024): 1-21. https://doi.org/10.30931/jetas.1169518.
JAMA
1.Ahmadi Dastgerdi K, Asadi D, Nabavi Chashmi SY, Tutsoy Ö. Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault. Journal of Engineering Technology and Applied Sciences. 2024;9:1–21.
MLA
Ahmadi Dastgerdi, Karim, vd. “Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault”. Journal of Engineering Technology and Applied Sciences, c. 9, sy 1, Nisan 2024, ss. 1-21, doi:10.30931/jetas.1169518.
Vancouver
1.Karim Ahmadi Dastgerdi, Davood Asadi, Seyed Yaser Nabavi Chashmi, Önder Tutsoy. Robust Adaptive Control Based on Incremental Nonlinear Dynamic Inversion for a Quadrotor in Presence of Partial Actuator Fault. Journal of Engineering Technology and Applied Sciences. 01 Nisan 2024;9(1):1-21. doi:10.30931/jetas.1169518