@article{article_619131, title={Non Simultaneous Morphing System Design for Yaw Motion in Quadrotors}, journal={Journal of Aviation}, volume={3}, pages={81–88}, year={2019}, DOI={10.30518/jav.619131}, author={Oktay, Tuğrul and Köse, Oğuz}, keywords={Quadrotor,Morphing,State Space Model,PID,Control}, abstract={<p class="MsoNormal" style="margin-top:6pt;margin-right:0cm;margin-bottom:6pt;margin-left:0cm;text-align:justify;line-height:115%;"> <span lang="en-us" style="font-size:10pt;line-height:115%;font-family:’Times New Roman’, serif;" xml:lang="en-us">Quadrotors are unmanned aerial vehicles that are
frequently used in military and civilian applications. In this study, the
modeling, control and variable geometry of the quadrotor’s yaw motion are
discussed non simultaneous. Quadrotor has a non-linner structure but the system
has been converted to linear structure by using various methods. Linear
expressions are expressed by state space model. Simulation was performed in
Matlab / Simulink environment using state space model. PID algorithm was used
as control system. In the simulations, both without morphing results and morphing
results were obtained and compared. </span> </p> <p> </p>}, number={2}, publisher={Vedat Veli ÇAY}