NMPC-Based Autopilot Design for Air-to-Air Missiles

In this paper, an overload autopilot based on generalized extended state observer, predictive function control and improved barrier interior-point method is designed to solve the problems of model nonlinearity, time variability and control constraints in attitude control of air-to-air missile. First...

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Autor principal: Cui Jiaming, Ma Kemao, Zhang Gongping
Formato: article
Lenguaje:ZH
Publicado: Editorial Office of Aero Weaponry 2021
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Acceso en línea:https://doaj.org/article/3b50e01c447f4979aec100389195ec10
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