Model reference tracking control of an aircraft: a robust adaptive approach
Makaleler > Tam Makale · 2016
Yazarlar: Ilker Tanyer, Enver TATLICIOĞLU, Erkan Zergeroglu
INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE, SCI Expanded İndekslerine Giren Dergi, Uluslararası, 2016, cilt 48, ss 1428-1437
DOI: 10.1080/00207721.2016.1261200
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.