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Adaptive attitude controller of a reentry vehicles based on Back-stepping Dynamic inversion method

This paper presents an attitude control algorithm for a Reusable Launch Vehicle (RLV) with a low lift/drag ratio (L/D < 0.5), in presence of external disturbances, model uncertainties, control output constraints and the thruster model. The main novelty of the proposed control strategy is a new combi...

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Autors principals: A. Mohseni, F. Fani Saberi, M. Mortazavi
Format: Artigo
Idioma:Inglês
Publicat: Amirkabir University of Technology 2018-06-01
Col·lecció:AUT Journal of Modeling and Simulation
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Accés en línia:https://miscj.aut.ac.ir/article_2669_f12d0b3e168755a10e53fcd1bbc6bb13.pdf
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