A Robust Dynamic Inversion Technique for Asymptotic Tracking Control of an Aircraft
Conference paper > Full Text · 2013
Authors: Ilker Tanyer, Enver TATLICIOĞLU, Erkan Zergeroglu
9th Asian Control Conference (ASCC), Turkey, İstanbul, International, Verbal, Full Text, 2013-2013, WoS, vol , pp 1-6
DOI: 10.1109/ascc.2013.6606263
Summary
In this paper, a tracking controller is developed for an aircraft model subject to uncertainties in the dynamics and additive state-dependent nonlinear disturbance-like terms. In the design of the controller, dynamic inversion technique is utilized in conjunction with a robust term. Only the output of aircraft dynamics is utilized in the controller design and acceleration measurements are not required. Lyapunov based stability analysis is used to prove global asymptotic tracking.