Yıl 2018, Cilt , Sayı 14, Sayfalar 269 - 271 2018-12-31

Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs)
Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs)

Sezer Çoban [1]

23 50

In this study, using dynamic model of passive and active morphing featured Tactical Unmanned Aerial Vehicle (TUAV)  called which is produced in Erciyes University, Faculty of Aeronautics and Astronautics, Model Aircraft Laboratory, under the TUBITAK ARDEB 1001 program and designing Output Constrained Variance Controller for aircraft tracking the desired trajectory achieved with minimal vibration and minimum energy consumption. For this purpose, using MATLAB, in the simulation environment, studies have been performed and closed loop responses have been obtained. Longitudinal motion is in primary interest, desired output is pitching angle of TUAV, and desired input is elevator angle.

In this study, using dynamic model of passive and active morphing featured Tactical Unmanned Aerial Vehicle (TUAV) called as ZANKA III which is produced in Erciyes University, Faculty of Aeronautics and Astronautics, Model Aircraft Laboratory, under the TUBITAK ARDEB 1001 program and designing Output Constrained Variance Controller for aircraft tracking the desired trajectory achieved with minimal vibration and minimum energy consumption. For this purpose, using MATLAB, in the simulation environment, studies have been performed and closed loop responses have been obtained. Longitudinal motion is in primary interest, desired output is pitching angle of TUAV, and desired input is elevator angle.

  • [1] R. Austin, Unmanned aircraft systems. Wiley, 2010.
  • [2] M. F. Bento, Unmanned aerial vehicles: An Overview. Working papers, 2008.
  • [3] Nelson, R. C. 2007. Flight Stability and Automatic Control. 2nd ed., McGraw-Hill, New York, chapters 2-6.
  • [4] Hsieh C., Skelton R. E. and Damra F. M., 1989, Minimum energy controllers with inequality constraints on output variances, Optimal Control Application and Methods, 10 (4), 347-366.
  • [5] Zhu G. and Skelton R E., 1991, Mixed and problems by weight selection in quadratic optimal control. International Journal of Quadratic Optimal Control, 63 (5) : 1161-1176.
Birincil Dil en
Konular Mühendislik
Dergi Bölümü Makaleler
Yazarlar

Orcid: 0000-0001-6750-5001
Yazar: Sezer Çoban (Sorumlu Yazar)
Kurum: ISKENDERUN TECHNICAL UNIVERSITY
Ülke: Turkey


Bibtex @araştırma makalesi { ejosat475870, journal = {Avrupa Bilim ve Teknoloji Dergisi}, issn = {}, eissn = {2148-2683}, address = {Osman Sağdıç}, year = {2018}, volume = {}, pages = {269 - 271}, doi = {10.31590/ejosat.475870}, title = {Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs)}, key = {cite}, author = {Çoban, Sezer} }
APA Çoban, S . (2018). Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs). Avrupa Bilim ve Teknoloji Dergisi, (14), 269-271. DOI: 10.31590/ejosat.475870
MLA Çoban, S . "Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs)". Avrupa Bilim ve Teknoloji Dergisi (2018): 269-271 <http://dergipark.gov.tr/ejosat/issue/40225/475870>
Chicago Çoban, S . "Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs)". Avrupa Bilim ve Teknoloji Dergisi (2018): 269-271
RIS TY - JOUR T1 - Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs) AU - Sezer Çoban Y1 - 2018 PY - 2018 N1 - doi: 10.31590/ejosat.475870 DO - 10.31590/ejosat.475870 T2 - Avrupa Bilim ve Teknoloji Dergisi JF - Journal JO - JOR SP - 269 EP - 271 VL - IS - 14 SN - -2148-2683 M3 - doi: 10.31590/ejosat.475870 UR - http://dx.doi.org/10.31590/ejosat.475870 Y2 - 2018 ER -
EndNote %0 Avrupa Bilim ve Teknoloji Dergisi Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs) %A Sezer Çoban %T Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs) %D 2018 %J Avrupa Bilim ve Teknoloji Dergisi %P -2148-2683 %V %N 14 %R doi: 10.31590/ejosat.475870 %U 10.31590/ejosat.475870
ISNAD Çoban, Sezer . "Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs)". Avrupa Bilim ve Teknoloji Dergisi / 14 (Aralık 2019): 269-271. http://dx.doi.org/10.31590/ejosat.475870