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Two approaches to simulating a group flight of unmanned aerial vehicles as system with lumped and distributed parameters

机译:两种模拟集总和分布参数的无人机群飞行系统的方法

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When using UAV groups to solve various problems, it is necessary to form a control that ensures the collection of the group with the construction of the required topology, as well as the control of each UAV within the framework of solving the general problem and preventing collisions in the group. The paper considers the theoretical and practical features of simulating the problem of controlling a large dense UAV group when it is establishing various types of the required topology using two possible approaches. The first – traditional – is based on the consideration of the UAV group as a set of individual participants (a system with lumped parameters), for each of which a control is formed that provides both a solution to the general problem and collision avoidance within the group. The second – proposed – is based on the consideration of the UAV group as a system with distributed parameters that are functions of time and spatial coordinates. The basis of this can serve as a consideration of the problems of kinematics and dynamics for systems of non-interacting closely spaced particles. Studies have shown the possibility of using the proposed approach. Advantages and disadvantages of this approach are noted.
机译:使用无人飞行器组解决各种问题时,有必要形成一种控制,以确保使用所需的拓扑结构来收集该组,并在解决一般问题和防止冲突的框架内控制每台无人飞行器在组中。本文考虑了当使用两种可能的方法建立各种类型的所需拓扑时,模拟控制大型稠密无人机的问题的理论和实践特征。第一种是传统的,是基于将UAV组视为一组单独的参与者(具有集总参数的系统)的考虑,针对每个参与者,都形成了一个控件,该控件既可以解决一般问题,又可以避免碰撞。团体。提出的第二个方案是基于对无人飞行器组作为具有时间和空间坐标的分布参数的系统的考虑。这样的基础可以作为非相互作用的紧密间隔粒子系统的运动学和动力学问题的考虑。研究表明,使用提议的方法的可能性。指出了此方法的优点和缺点。

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