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The design and simulation of unmanned aerial vehicles (UAVs) have gained significant attention due to their diverse applications in various fields, including surveillance, reconnaissance, environmental monitoring, disaster response, and logistics, this kind of activity suggest that human officers or individual personnel will be able to monitor remotely, live streaming and acquiring specific data from the aerial vehicle while planning or evaluating their operations. In addition, UAV simulations extend to flight dynamics and control systems, where mathematical models and algorithms are developed to mimic real-world behaviors. These simulations enable the assessment of flight performance, and responsiveness, aiding in the development of control strategies. Simulation plays a pivotal role in refining the UAV design before physical fabrication and testing. Plotting in MATLAB R2023A 2016a software was used to create detailed 3D models of the UAV and the 6 degrees of freedom in a signal form, with the specifications of maximum roll angle 500, pitch angle 300, and tilt angle 350, which enabling precise visualization and manipulation of components. Aerodynamic simulations, often conducted using computational fluid dynamics (CFD), provide insights into the aircraft's flight characteristics, stability, and control. Structural analysis simulations evaluate the integrity of the airframe under various load conditions. The simulation shows a very stable operation through an interdisciplinary approach and state-of-the-art simulation tools. The UAV's performance, stability, and safety were evaluated, allowing for iterative refinements in the design. The presented methodology serves as a valuable foundation for the development of cutting-edge UAV technologies that can thrive in diverse operational scenarios.
SANUSI et al. (Sat,) studied this question.