Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Imil Hamda Imran"'
Autor:
Taiba Kouser, Dilek Funda Kurtulus, Abdulrahman Aliyu, Srikanth Goli, Luai M. Alhems, Imil Hamda Imran, Azhar M. Memon
Publikováno v:
IEEE Access, Vol 12, Pp 83658-83674 (2024)
In the present study, numerical simulation for a two-dimensional NACA0005 is performed for angles of attack ${\alpha } = {0^{\circ }-15^{\circ }}$ . The Reynolds numbers 1000, 2000 and 5000 are considered. Simulations show that the flow fields can be
Externí odkaz:
https://doaj.org/article/8bf890a365474d609cc8ec58b01146f3
Autor:
Imil Hamda Imran, Dilek Funda Kurtulus, Azhar M. Memon, Srikanth Goli, Taiba Kouser, Luai Muhammad Alhems
Publikováno v:
IEEE Access, Vol 12, Pp 55326-55341 (2024)
This paper investigates the formation control of multiple heterogeneous quadrotor unmanned aerial vehicles (UAVs). The research focuses on developing a distributed robust formation control strategy to effectively manage the translational and attitude
Externí odkaz:
https://doaj.org/article/06a9c782d93b4e1e9c556265a6fb0481
Publikováno v:
Scientific Reports, Vol 13, Iss 1, Pp 1-15 (2023)
Abstract Stainless steel (SS) is widely employed in industrial applications that demand superior corrosion resistance. Modeling its corrosion behavior in common structural and various operational scenarios is beneficial to provide wall-thickness (WT)
Externí odkaz:
https://doaj.org/article/57c6c34567624343b63838a05312ce01
Publikováno v:
Mathematics, Vol 12, Iss 11, p 1767 (2024)
The paper introduces a robust adaptive fault-tolerant control system for the six-degree-of-freedom (six-DOF) dynamics of quadrotor unmanned aerial vehicles (UAVs), incorporating disturbances and abrupt actuator faults to represent real-world conditio
Externí odkaz:
https://doaj.org/article/888e3db776644a4c89912a210d63a77f
Publikováno v:
Proceedings of Engineering and Technology Innovation (2023)
This study aims to the utilization of vortex structures generated through wing flapping for achieving sustainable flight, and the motivation is elicited by the phenomenon observed in natural flyers. The vortex structures in the flow field generated b
Externí odkaz:
https://doaj.org/article/4f66a16cc3c941d4b3803499ebcdf162
Publikováno v:
Results in Engineering, Vol 20, Iss , Pp 101555- (2023)
The usage of multicopter unmanned aerial vehicles (UAVs) has increased for various military and civilian purposes. The choice of propulsion system of such a vehicle is crucial to fulfill the intended mission requirements. The present study focuses on
Externí odkaz:
https://doaj.org/article/c18d3354b9c34a4896a7a37483bf3af8
Publikováno v:
Scientific Reports, Vol 13, Iss 1, Pp 1-19 (2023)
Abstract The real-time unknown parameter estimation and adaptive tracking control problems are investigated in this paper for a six degrees of freedom (6-DOF) of under-actuated quadrotor unmanned aerial vehicle (UAV). A virtual proportional derivativ
Externí odkaz:
https://doaj.org/article/4b3ae9f962db4c06a04339985eccdcdb
Publikováno v:
IEEE Access, Vol 11, Pp 55630-55643 (2023)
The discrete control problem of vertical take-off and landing unmanned aerial vehicle (VTOL UAV) in the presence of time-varying uncertain disturbances is developed in this paper. The complexity of control problem is managed by dividing the dynamical
Externí odkaz:
https://doaj.org/article/fd6a7817f4c0491a9847ae00d1226f5f
Publikováno v:
IEEE Access, Vol 11, Pp 19710-19724 (2023)
This paper studies the real-time parameter estimation and adaptive tracking control problem for a six degrees of freedom (6-DOF) of quadrotor unmanned aerial vehicle (UAV) as an under-actuated system. A virtual proportional derivative (PD) is propose
Externí odkaz:
https://doaj.org/article/253130338c324b3d9a842681b785514d
In this paper, a centralised robust discrete-time sliding mode controller is proposed for the formation control of a multi-quadrotor system in the presence of disturbances. The control system, based on consensus control, is designed around the full,
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e54fa60d5914cf8e0c37accf027a49f5
https://doi.org/10.1016/j.ifacol.2022.10.184
https://doi.org/10.1016/j.ifacol.2022.10.184