Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Ilker Tanyer"'
Publikováno v:
Archives of Control Sciences, Vol vol. 31, Iss No 2, Pp 267-286 (2021)
In this paper, model reference output feedback tracking control of an aircraft subject to additive, uncertain, nonlinear disturbances is considered. In order to present the design steps in a clear fashion: first, the aircraft dynamics is temporarily
Externí odkaz:
https://doaj.org/article/d8a8af464250449180ee15a71eb3f9b5
Publikováno v:
International Journal of Robotics and Automation. 35
Publikováno v:
International Journal of Systems Science. 48:1428-1437
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 nonl
Autor:
Enver Tatlicioglu, Meryem Deniz, Erkan Zergeroglu, Alper Bayrak, Ilker Tanyer, Barbaros Özdemirel
Publikováno v:
IET Control Theory & Applications. 10:1612-1619
In this study, an asymptotic tracking controller is developed for an aircraft model subject to additive, state-dependent, non-linear disturbance-like terms. Dynamic inversion technique in conjunction with robust integral of the sign of the error term
Publikováno v:
IFAC Proceedings Volumes. 47:3202-3207
19th IFAC World Congress on International Federation of Automatic Control, IFAC 2014; Cape Town; South Africa; 24 August 2014 through 29 August 2014
This work presents, the design and the corresponding analysis of a nonlinear controller for an a
This work presents, the design and the corresponding analysis of a nonlinear controller for an a
Publikováno v:
ASCC
9th Asian Control Conference, ASCC 2013; Istanbul; Turkey; 23 June 2013 through 26 June 2013
In this paper, a tracking controller is developed for an aircraft model subject to uncertainties in the dynamics and additive state-dependent nonlinear
In this paper, a tracking controller is developed for an aircraft model subject to uncertainties in the dynamics and additive state-dependent nonlinear
Publikováno v:
SIU
In this study, a nonlinear control technique that guarantee exponential output tracking for unmanned aerial vehicles subject to uncertainties in system dynamics and additive nonlinear disturbances is developed. In the literature, dynamic inversion me
Publikováno v:
2009 IEEE 17th Signal Processing and Communications Applications Conference.
In this paper, Consistency Analysis of Kalman Filter for Modal Analysis of Structural Systems is made. As a future work, A fundamental Modal Analysis algorithm, Eigensystem Realization Algorithm(ERA) will be used with Kalman filters together to make