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Abstract

This paper proposes a finite-time horizon suboptimal control strategy based on statedependent 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.
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Authors and Affiliations

Marcin Chodnicki
1
Paweł Pietruszewski
1
Mariusz Wesołowski
1
Sławomir Stępień
2

  1. Air Force Institute of Technology, Ksiecia Bolesława 6, 01-494 Warsaw, Poland
  2. Poznan University of Technology, Institute of Automatic Control and Robotics, Piotrowo 3a, 60-965 Poznan, Poland

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