A robust dynamic inversion technique for asymptotic tracking control of an aircraft
| Autor: | Enver Tatlicioglu, Ilker Tanyer, Erkan Zergeroglu |
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| Přispěvatelé: | TR123720, Tanyer, İlker, Tatlıcıoğlu, Enver, Izmir Institute of Technology. Electronics and Communication Engineering |
| Rok vydání: | 2013 |
| Předmět: |
Controller design
Lyapunov function Engineering Adaptive control Controllers business.industry Control engineering Inversion (meteorology) Controller designs Vehicle dynamics symbols.namesake Nonlinear system Aircraft dynamics Exponential stability Control theory symbols Robust dynamic inversions business Global asymptotic tracking Aircraft models |
| Zdroj: | ASCC |
| Popis: | 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 disturbance-like terms. In the design of the controller, dynamic inversion technique is utilized in conjuction 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. © 2013 IEEE. |
| Databáze: | OpenAIRE |
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