Design of a Linear Quadratic Optimal Control for Aircraft Flight Control by Genetic Algorithm

نویسندگان

  • J. Aranda
  • J. M. de la Cruz
  • M. Parrilla
  • P. Ruipérez
چکیده

In this paper we have investigated the use of genetic algorithm for the selection of weighting matrices of performance index for the linear quadratic control design. We can easily consider in the fitness index of the genetic algorithm different design specifications and their verifications in different operations conditions. As well as a measure of robustness σ(S+T) evaluated at the input and at the output for linearized models obtained for different parameters. This technique is applied to design a control for the longitudinal dynamic of an aircraft. The robustness and specifications are evaluated for different values of mass, airspeed, centre of gravity, and transport delay.

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تاریخ انتشار 2000