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Adaptive Attitude Control for Multi-MUAV Systems With Output Dead-Zone and Actuator Fault 被引量:9
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作者 Guowei Dong Liang Cao +2 位作者 Deyin Yao Hongyi Li Renquan Lu 《IEEE/CAA Journal of Automatica Sinica》 SCIE EI CSCD 2021年第9期1567-1575,共9页
Many mechanical parts of multi-rotor unmanned aerial vehicle(MUAV)can easily produce non-smooth phenomenon and the external disturbance that affects the stability of MUAV.For multi-MUAV attitude systems that experienc... Many mechanical parts of multi-rotor unmanned aerial vehicle(MUAV)can easily produce non-smooth phenomenon and the external disturbance that affects the stability of MUAV.For multi-MUAV attitude systems that experience output dead-zone,external disturbance and actuator fault,a leader-following consensus anti-disturbance and fault-tolerant control(FTC)scheme is proposed in this paper.In the design process,the effect of unknown nonlinearity in multi-MUAV systems is addressed using neural networks(NNs).In order to balance out the effects of external disturbance and actuator fault,a disturbance observer is designed to compensate for the aforementioned negative impacts.The Nussbaum function is used to address the problem of output dead-zone.The designed fault-tolerant controller guarantees that the output signals of all followers and leader are synchronized by the backstepping technique.Finally,the effectiveness of the control scheme is verified by simulation experiments. 展开更多
关键词 Disturbance observer fault-tolerant control(FTC) multi multi-rotor unmanned aerial vehicle(multi-MUAV)attitude systems neural networks(NNs) output dead-zone
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