Longitudinal motion is in primary interest, desired output is pitching angle of TUAV, and desired input is elevator angle.
📌 3 Key Takeaways
🎯
Objective & Hypothesis:In this study, using dynamic model of passive and active morphing featured Tactical Unmanned Aerial Vehicle (TUAV) calledwhich is produced in Erciyes University, Faculty of Aeronautics and Astronautics, Model Aircraft Laboratory, under theTUBITAK ARDEB 1001 program and designing Output Constrained Variance Controller for aircraft tracking the desiredtrajectory achieved with minimal vibration and minimum energy consumption.
📊
Key Findings & Data:For this purpose, using MATLAB, in thesimulation environment, studies have been performed and closed loop responses have been obtained.
💡
Conclusion & Impact:Longitudinal motion is in primary interest, desired output is pitching angle of TUAV, and desired input is elevator angle.
🔬Design:Modeling & Simulation
📍Scope:Comprehensive Sample
⚙️Variables:Domain Parameters
Abstract
In this study, using dynamic model of passive and active morphing featured Tactical Unmanned Aerial Vehicle (TUAV) calledwhich is produced in Erciyes University, Faculty of Aeronautics and Astronautics, Model Aircraft Laboratory, under theTUBITAK ARDEB 1001 program and designing Output Constrained Variance Controller for aircraft tracking the desiredtrajectory achieved with minimal vibration and minimum energy consumption. For this purpose, using MATLAB, in thesimulation 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.
🔖
Cite This Article
ÇOBAN, S. (2022). Variance Constrained Vibration Control of Morphing Tactical Unmanned Aerial Vehicles (TUAVs). Avrupa Bilim ve Teknoloji Dergisi, Cilt: 0 - Sayı: 14, 269–271. https://ajindex.com/articles/458319
R. Austin, Unmanned aircraft systems. Wiley, 2010.
M. F. Bento, Unmanned aerial vehicles: An Overview. Working papers, 2008.
Nelson, R. C. 2007. Flight Stability and Automatic Control. 2nd ed., McGraw-Hill, New York, chapters 2- 6. 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. 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.