A fault-tolerant control method for distributed flight control system facing wing damage

نویسندگان

چکیده

With the strong battlefield application environment of next generation fighter, based on design distributed vehicle management system, a fault diagnosis and fault-tolerant control (FTC) method for wing surface damage is proposed in this paper. Aiming at three kinds modes, paper proposes decision tree forms from aspects sample database construction, feature parameter extraction, construction. Based results, longitudinal law dynamic inverse lateral-directional robust laws linear quadratic regulator (LQR) are proposed. From simulation examples, algorithm can complete judgment modes within 2 ms, FTC make fighter quickly return to stable flight state after short transient 1 s, which achieves goal.

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ژورنال

عنوان ژورنال: Chinese Journal of Systems Engineering and Electronics

سال: 2021

ISSN: ['1004-4132']

DOI: https://doi.org/10.23919/jsee.2021.000089