Concept of anti-collision algorithm for unmanned aerial vehicles

Sebastian Tatko, S. Konatowski
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Abstract

The basis of the novel anti-collision algorithm is a software implementation that allows theUAV to avoid collisions with environmental obstacles, as well as with other flying objects. The paperuses simplified equations describing the dynamics of the quadcopter to facilitate the modelling ofthe simulation structure. The software implementation of the quadcopter model together with thecontroller is the basis for the operation of the anti-collision algorithm. The model control system usesa three-stage proportional-integral-differential controller. The inspiration of the resulting program ismagnetic interaction. The obstacle avoidance algorithm is based on the measurement of angular valuesand the selection of a proportional virtual force. The force repelling a quadcopter from an obstacle isa parameter that depends on its linear velocity, bearing on the obstacle and distance to the obstacle.The heat maps obtained reflect the scaling of the value and direction of the repulsive force. Afterdefining the target point and the position of the obstacle, the necessary parameters are measured andthe collision course correcting coordinates are selected on-board the quadcopter. The flight parametersof the quadcopter and the control coefficients of the anti-collision algorithm were analysed. Thecorrectness of the programs operation was checked by simulation using numerous characteristics.Keywords: Unmanned Aerial Vehicle, obstacle avoidance, anti-collision algorithm, UAV dynamicsmodel, quadcopter
无人机防碰撞算法的概念
新型防碰撞算法的基础是一个软件实现,允许无人机避免与环境障碍物以及与其他飞行物体的碰撞。本文采用简化的四轴飞行器动力学方程,便于对仿真结构进行建模。四轴飞行器模型与控制器的软件实现是防碰撞算法运行的基础。模型控制系统采用三级比例-积分-微分控制器。由此产生的程序的灵感是磁相互作用。避障算法是基于角度值的测量和比例虚拟力的选择。使四轴飞行器远离障碍物的力是一个参数,它取决于飞行器的线速度、与障碍物的关系以及与障碍物的距离。得到的热图反映了排斥力的大小和方向的缩放。在确定目标点和障碍物位置后,在四轴飞行器上测量必要的参数并选择碰撞轨迹校正坐标。分析了四轴飞行器的飞行参数和防撞算法的控制系数。利用多种特性进行仿真,验证了程序运行的正确性。关键词:无人机,避障,防碰撞算法,无人机动力学模型,四轴飞行器
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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