3825. A Study of a Moving Mass Coaxial Monocopter
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Paper
Abstract
The evolution of aerial drone technology has led to a growing interest in innovative configurations that optimize efficiency and maneuverability. Among these, monocopters have emerged as a promising alternative to traditional quadcopters, offering higher thrust-to-loading area ratios and reduced mechanical complexity. This paper presents the design, simulation, and control strategies for a novel moving mass coaxial monocopter. By leveraging the concept of moving mass control, which dynamically adjusts the center of mass to achieve precise orientation and trajectory adjustments, this monocopter design eliminates the need for complex stabilization mechanisms. The study explores the structural design and aerodynamic advantages of the proposed configuration, emphasizing its potential for lightweight, energy-efficient, and long-endurance missions. A comprehensive simulation framework is developed to analyze the nonlinear dynamics of the system to address associated challenges. The findings highlight the moving mass coaxial monocopter’s capability to maintain stability and maneuverability in diverse flight conditions, offering a versatile solution for applications requiring rapid responsiveness and extended operational duration.
