Methodology for the Synthesis of a Multicopter Controller Acting as a Swarm Agent using the Thermal Motion Equivalent Method

Q4 Engineering
E. Heiss, O. Morozov, A. Kozyr, A. G. Efromeev
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Abstract

The paper is dedicated to the development of a method for the synthesis of the control system of a swarm multicopter. The motion of the agents in the swarm is organised by the thermal motion equivalent method. The idea of the method is the behavioral similarity of the thermal motion of the atoms by the agents. In the practical implementation of the thermal motion equivalent method, it is important to ensure constancy of velocity and isotropy of agent dynamics. Violating these properties will cause the swarm to fail a mission, such as an area exploration, by reducing the RMS speed of the agents to zero. The proposed solution to these problems is to synthesize a modal controller for the agent-boundaries test system for the slowest control channel, thereby ensuring RMS velocity constancy of the agent. The synthesized controller is used as a filter in the fast-acting channels, the second horizontal channel and the vertical channel. In the fast-acting channels, an additional filter is proposed to bring their dynamics to the slowest channel, thereby ensuring isotropy. The inclusion of a limit on the maximum length of the equivalent field vector ensures isotropy. The synthesis was carried out using a simplified multicopter dynamics mathematical model, obtained with small UAV deviations from the vertical and without considering the Coriolis force. The methodology for the synthesis of a multicopter control system for functioning as part of a swarm is developed using the obtained results. Numerical simulation results of both a single vehicle in closed space and a swarm using a more complete nonlinear dynamic quadcopter model are presented. The proposed method has the advantage of simple synthesis using a linear model. Numerical simulation results confirm the operability of the developed methodology.
利用热运动等效法合成作为蜂群代理的多旋翼飞行器控制器的方法论
本文致力于开发一种合成蜂群多旋翼飞行器控制系统的方法。蜂群中代理的运动是由热运动等效方法组织的。该方法的理念是代理原子热运动的行为相似性。在热运动等效法的实际应用中,必须确保速度的恒定性和代理动态的各向同性。违反这些特性将导致虫群无法完成任务,如区域探索,因为虫群的有效值速度会降为零。针对这些问题提出的解决方案是为最慢控制通道的代理-边界测试系统合成一个模态控制器,从而确保代理的均方根速度恒定。合成控制器在快速通道、第二水平通道和垂直通道中用作滤波器。在快速通道中,建议使用额外的滤波器,使其动态特性与最慢通道一致,从而确保各向同性。对等效场矢量最大长度的限制也确保了各向同性。合成是使用简化的多旋翼飞行器动力学数学模型进行的,该模型是在无人驾驶飞行器偏离垂直方向较小且不考虑科里奥利力的情况下获得的。利用所获得的结果,制定了多旋翼飞行器控制系统的合成方法,使其作为飞行群的一部分发挥作用。介绍了封闭空间中单个飞行器和使用更完整的非线性动态四旋翼模型的蜂群的数值模拟结果。所提出的方法具有使用线性模型进行简单合成的优点。数值模拟结果证实了所开发方法的可操作性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Mekhatronika, Avtomatizatsiya, Upravlenie
Mekhatronika, Avtomatizatsiya, Upravlenie Engineering-Electrical and Electronic Engineering
CiteScore
0.90
自引率
0.00%
发文量
68
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