Finite-time SDRE control of F16 aircraft dynamics

• Autorzy: Chodnicki Marcin , Pietruszewski Paweł , Wesołowski Mariusz , Stępień Sławomir

Identyfikatory

DOI

10.24425/acs.2022.142848

• Języki publikacji: EN

Abstrakty

EN

This paper proposes a finite-time horizon suboptimal control strategy based on state-dependent Riccati equation (SDRE) to control of F16 multirole aircraft. Flight stabilizer control of super maneuverable aircraft is modelled and simulated. For aircraft modelling purpose a full 6 DOF model is considered and described by nonlinear state-space approach. Also a stable state-dependent parametrization (SDP) necessary for solution of the SDRE control problem is proposed. Solution of the SDRE control problem with adequate defined weighting matrices in performance index shows possibility of fast and optimal aircraft control in finite-time. The method in this form can be used for stabilization of aircraft flight and aerodynamics.

Słowa kluczowe

EN

aircraft modelling; state-dependent Riccati equations; finite-time optimal control

• Wydawca: Polish Academy of Sciences, Committee of Automatic Control and Robotics
• Czasopismo: Archives of Control Sciences
• Rocznik: 2022
• Tom: Vol. 32, No. 3
• Strony: 557--576
• Opis fizyczny: Bibliogr. 37 poz., rys., tab., wykr., wzory

Twórcy

autor

Chodnicki Marcin

• Air Force Institute of Technology, Księcia Bolesława 6, 01-494 Warsaw, Poland

autor

Pietruszewski Paweł

• Air Force Institute of Technology, Księcia Bolesława 6, 01-494 Warsaw, Poland

autor

Wesołowski Mariusz

• Air Force Institute of Technology, Księcia Bolesława 6, 01-494 Warsaw, Poland

autor

Stępień Sławomir

• Poznan University of Technology, Institute of Automatic Control and Robotics, Piotrowo 3a, 60-965 Poznań, Poland

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Uwagi

Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023)