Conference
A robust dynamic inversion technique for asymptotic tracking control of an aircraft
| العنوان: | A robust dynamic inversion technique for asymptotic tracking control of an aircraft |
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| المؤلفون: | Tanyer, İlker, Tatlıcıoğlu, Enver, Zergeroğlu, Erkan |
| بيانات النشر: | Institute of Electrical and Electronics Engineers Inc. |
| سنة النشر: | 2013 |
| مصطلحات موضوعية: | Controllers, Aircraft models, Controller designs, Global asymptotic tracking, Robust dynamic inversions |
| جغرافية الموضوع: | 10.1109/ASCC.2013.6606263 |
| الوصف: | 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. |
| نوع الوثيقة: | conference object |
| اللغة: | English |
| ردمك: | 978-1-4673-5769-2 1-4673-5769-3 |
| Relation: | 9th Asian Control Conference, ASCC 2013; Konferans Öğesi - Uluslararası - Kurum Öğretim Elemanı; Tanyer, İ., Tatlıcıoğlu, E., and Zergeroğlu, E. (2013, June 23-26). A robust dynamic inversion technique for asymptotic tracking control of an aircraft. Paper presented at the 9th Asian Control Conference. doi:10.1109/ASCC.2013.6606263; http://doi.org/10.1109/ASCC.2013.6606263; http://hdl.handle.net/11147/5256; WOS:000333734900274; 2-s2.0-84886509619 |
| DOI: | 10.1109/ASCC.2013.6606263 |
| الاتاحة: | http://hdl.handle.net/11147/5256 https://doi.org/10.1109/ASCC.2013.6606263 |
| Rights: | open |
| رقم الانضمام: | edsbas.CF1EC754 |
| قاعدة البيانات: | BASE |
| ردمك: | 9781467357692 1467357693 |
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| DOI: | 10.1109/ASCC.2013.6606263 |