Permanent Magnet Synchronous Motors (PMSMs) have garnered sustained attention over the past four decades due to their high efficiency, superior torque density, and dependable operational characteristics, making them highly suitable for a wide range of industrial applications. Accurate dynamic modelling of PMSMs is essential for performance evaluation and the development of advanced drive control strategies. Although previous studies have addressed customized modelling approaches for various PMSM types, a streamlined method for deriving model parameters from standard manufacturer specifications remains insufficiently explored. As a result, simulation studies are often disconnected from commercially available motor data, thereby limiting their practical relevance. In this study, the dynamic model of a PMSM is reformulated within the synchronous rotating reference frame (d-q axis) and implemented using mathematical function blocks in the MATLAB/Simulink environment. A systematic procedure is developed to extract key motor parameters from typical manufacturer data sheets. This approach bridges the gap between theoretical modeling and real-world motor implementation. The proposed modelling framework is validated using a standard 1 hp, 2.2 Nm, 1500 rpm PMSM, and its performance is benchmarked against the built-in Simulink PMSM blockset. Simulations are conducted to evaluate the mechanical output, rotor speed, and electromagnetic torque responses under step variations in load torque. The results exhibited strong agreement between the custom mathematical model and the blockset counterpart, confirming the accuracy and practical applicability of the parameter extraction methodology.
Flapping wing robots (FWRs), inspired by the complex aerodynamics of birds, insects, and bats, have garnered substantial interest in recent years due to their ability to replicate agile and energy-efficient flight behaviors observed in nature. These biologically inspired aerial platforms are capable of executing sophisticated maneuvers, including stable hovering and rapid directional changes, which are typically unattainable by conventional rotary or fixed-wing aircraft. Attitude control systems, which are essential for ensuring flight stability across diverse environmental conditions, have undergone significant advancements with the integration of lightweight materials, novel actuation mechanisms, and miniaturized sensory technologies. Despite these developments, challenges persist in achieving robust, energy-efficient flight control under dynamically changing aerodynamic conditions. Bio-mimetic sensor technologies, such as gyroscopes, accelerometers, and tactile feedback systems, have been increasingly adopted to enable closed-loop feedback and real-time adaptive control. Both open-loop and closed-loop architectures have been investigated, with a growing emphasis on adaptive and learning-based control strategies to accommodate nonlinear flight dynamics. Recent research has explored the incorporation of artificial intelligence (AI) and machine learning (ML) algorithms to enhance autonomy, environmental adaptability, and decision-making capabilities. Despite these advances, limitations persist in power management, environmental robustness, and long-term flight endurance. Potential applications in surveillance, environmental monitoring, precision agriculture, and search-and-rescue missions underscore the transformative value of FWRs within autonomous aerial systems. Through continued interdisciplinary research in materials science, control theory, and computational intelligence, FWRs are anticipated to emerge as a pivotal class within the broader ecosystem of autonomous aerial systems.