Adaptive Control for an Aircraft Wing System with Hysteresis Nonlinearity
نویسندگان
چکیده
This paper involves a novel adaptive control approach of flexible wing system with hysteresis nonlinearity. The usual design strategies based on the ordinary differential equations (ODEs) are inapplicable due to described in partial (PDEs), and algorithm becomes highly intricate. Firstly, inverse dynamic model is introduced compensate for Considering unknown external disturbances, an technique utilized compensation. Then, direct Lyapunov employed prove bounded stability system. Lastly, effectiveness proposed validated via simulation results.
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ژورنال
عنوان ژورنال: Mathematics
سال: 2023
ISSN: ['2227-7390']
DOI: https://doi.org/10.3390/math11183841