DOAJ Open Access 2022

Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method

Yuwei Cui Aijun Li Biao Duan Shabbir Wasif

Abstrak

The paper concentrates on the problem of fault-tolerant control of UAV against actuator faults from the perspective of flight control system architecture. Using backstepping control method and inverse optimization theory, the design of backstepping optimal control law was constructed. Based on the fault monitoring mechanism of vehicle management computer in the distributed flight control and control allocation system, a fault-tolerant control design method was established in the case of multiple failure modes of the actuators, which compensates the influence caused by the failures. Finally, the effectiveness of the proposed strategy was verified by numerical simulation.

Topik & Kata Kunci

Motor vehicles. Aeronautics. Astronautics

Penulis (4)

Yuwei Cui

Aijun Li

Biao Duan

Shabbir Wasif

Format Sitasi

APA MLA BibTeX

Cui, Y., Li, A., Duan, B., Wasif, S. (2022). Reconfiguration Control Design of UAV against Actuator Faults Based on Control Allocation Method. https://doi.org/10.1155/2022/4481553

Akses Cepat

PDF tidak tersedia langsung

Cek di sumber asli →

Lihat di Sumber doi.org/10.1155/2022/4481553

Informasi Jurnal

Tahun Terbit: 2022
Sumber Database: DOAJ
DOI: 10.1155/2022/4481553
Akses: Open Access ✓