Effect of marginal variation of aspect ratio and frequency with kinematic asymmetry on flow field around flapping rigid wing in hover by Srikanth Goli, Arnab Roy, Subhransu Roy

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Evolution of Vortex Structures Generated by a Rigid Flapping Wing with a Winglet in Quiescent Water by Srikanth Goli, Arnab Roy, Subhransu Roy, Imil Hamda Imran

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Experimental study on efficient propulsion system for multicopter UAV design applications by Srikanth Goli, Dilek Funda Kurtuluş, Luai M. Alhems, Azhar M. Memon, Imil Hamda Imran

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Extended Discrete-Time Quasi-Sliding Mode Control for VTOL UAV in the Presence of Uncertain Disturbances by Imil Hamda Imran, Azhar M. Memon, Dilek Funda Kurtulus, Srikanth Goli, Luai Muhammad Alhems

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Distributed Robust Formation Control of Heterogeneous Multi-UAVs With Disturbance Rejection by Imil Hamda Imran, Dilek Funda Kurtulus, Azhar M. Memon, Srikanth Goli, Taiba Kouser, Luai Muhammad Alhems

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