Year 2018, Volume , Issue 14, Pages 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]


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.

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  • [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.
Primary Language en
Subjects Engineering
Journal Section Makaleler
Authors

Orcid: 0000-0001-6750-5001
Author: Sezer Çoban (Primary Author)
Institution: ISKENDERUN TECHNICAL UNIVERSITY
Country: Turkey


Dates

Publication Date : December 31, 2018

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