Landing control design for a VTOL aircraft
نویسندگان
چکیده
منابع مشابه
Robust Fault Tolerant Tracking Controller Design for a VTOL aircraft
This paper deals with the fault tolerant control (FTC) design for a Vertical Takeoff and Landing (VTOL) aircraft subject to external disturbances and actuator faults. The aim is to synthesize a fault tolerant controller ensuring trajectory tracking for the nonlinear uncertain system represented by Takagi-Sugeno (T-S) model. In order to design the FTC law, a proportional integral observer (PIO) ...
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ژورنال
عنوان ژورنال: IET Control Theory & Applications
سال: 2020
ISSN: 1751-8652,1751-8652
DOI: 10.1049/iet-cta.2018.6244