Observer based rotor failure compensation for biplane quadrotor with slung load

نویسندگان

چکیده

In this study, mathematical modeling of biplane quadrotor with slung load is proposed. Performance the degrade while swinging so to compensate it nonlinear observer based backstepping controller designed that can not only handle disturbance generated by but also capable tackle partial rotor failure and wind gust. Simulation study carried out considering (only for mode), gust, (for all three modes) as external design estimate it. Backstepping control technique used modes quadrotor. shows proposed scheme cable different sources in biplane.

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ژورنال

عنوان ژورنال: Ain Shams Engineering Journal

سال: 2022

ISSN: ['2090-4479', '2090-4495']

DOI: https://doi.org/10.1016/j.asej.2022.101748