Adaptive Fault-Tolerant H-Infinity Output Feedback Control for Lead–Wing Close Formation Flight
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DOI: 10.1109/tsmc.2018.2830511
Abstract: This paper investigates the attitude and position tracking control problem of the Lead–Wing close formation system with unknown multiplicative actuator faults. In close formation flight, the movement of the Wing unmanned aerial vehicle (UAV) is… read more here.
Keywords: lead wing; control; formation; close formation ... See more keywords