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Analysis of Wing Twist Effects on Hover Flight Dynamics of a Single Rotor Aerial Craft
Conference proceeding

Analysis of Wing Twist Effects on Hover Flight Dynamics of a Single Rotor Aerial Craft

Jun En Low, Ying Hong Pheh, Shaohui Foong and IEEE
IEEE/ASME International Conference on Advanced Intelligent Mechatronics, pp.323-328
IEEE ASME International Conference on Advanced Intelligent Mechatronics
01/01/2016

Abstract

Automation & Control Systems Computer Science Computer Science, Artificial Intelligence Engineering Engineering, Electrical & Electronic Robotics Science & Technology Technology
Advancements in control theory and the miniaturization of microelectronics has led to significant improvements in the aerial characteristics and performance of single rotor aerial crafts. These single rotor aerial crafts are of particular interest as they can be considered true hybrids between traditional fixed-wing crafts and the maneuverable multi-rotor platforms, allowing both VTOL capabilities as well as extended endurance. Currently, the dynamic models used to describe these novel crafts are hindered by the lack of an optimized wing design that caters to the single rotor aerial craft's unique flight envelope. Hence, this paper seeks to investigate and explore wing models with specific twist angles across the wingspan so as to improve the craft's hover performance and in turn, its endurance. Simulation results suggest that for the wing twist characteristic, a reciprocal function model outperforms linear function models in terms of induced power loss without incurring any significant drawbacks to existing design setups. With the advent of digital fabrication, such customized and intricate wing designs can be more easily realized.

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