Model reference tracking control of an aircraft: a robust adaptive approach


Tanyer I., Tatlicioglu E. , Zergeroglu E.

INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, cilt.48, ss.1428-1437, 2017 (SCI İndekslerine Giren Dergi) identifier identifier

  • Cilt numarası: 48
  • Basım Tarihi: 2017
  • Doi Numarası: 10.1080/00207721.2016.1261200
  • Dergi Adı: INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE
  • Sayfa Sayıları: ss.1428-1437

Özet

This work presents the design and the corresponding analysis of a nonlinear robust adaptive controller for model reference tracking of an aircraft that has parametric uncertainties in its system matrices and additive state-and/or time-dependent nonlinear disturbance-like terms in its dynamics. Specifically, robust integral of the sign of the error feedback term and an adaptive term is fused with a proportional integral controller. Lyapunov-based stability analysis techniques are utilised to prove global asymptotic convergence of the output tracking error. Extensive numerical simulations are presented to illustrate the performance of the proposed robust adaptive controller.