Adaptive fuzzy direct lift control of aircraft carrier-based landing

نویسندگان

چکیده

Considering the precise landing demand for carrier-based aircraft flight control, this paper proposes an adaptive fuzzy control method strong time-varying, parameter uncertainty and various complex coupling in actual state model. This is applied to flap channel achieve direct lift system utilized approximate six-degree-of-freedom nonlinear model of a carrier that difficult accurately describe, accurate tracking glideslope, improve accuracy. Lyapunov was used judge stability algorithm. During simulation, airwake deck motion disturbance were introduced simulate environment aircraft. The effectiveness verified by Matlab software. Monte-Carlo random test carry out point accuracy conventional scheme respectively. Through response curve statistical results, it confirmed has better effect, precision improvement compared with scheme.

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ژورنال

عنوان ژورنال: Xibei gongye daxue xuebao

سال: 2021

ISSN: ['1000-2758', '2609-7125']

DOI: https://doi.org/10.1051/jnwpu/20213920359