Performance-Constraint Fault Tolerant Control to Aircraft in Presence of Actuator Deviation
Peng Tang,
Chuangxin Zhao,
Shizhe Liang
et al.
Abstract:Accuracy of electro-mechanical actuator in aircraft is susceptible to variable operation conditions such as electromagnetic interference, changeable temperature or loss of maintenance, leading in turn to flight performance degradation. This paper proposed an unified control paradigm that aims to keep aircraft’s velocity in a safe boundary and shorten the system stabilizing time in presence of actuator deviation. The controller is derived following a practical finite-time-convergence (FTC) with extended dynamic… Show more
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