Flight control and collision avoidance of three UAVs following each other

Q2 Engineering
Z. Kutpanova, H. Temeltas, S. Kulmamirov
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引用次数: 0

Abstract

An unmanned aerial vehicle is a hardware and software complex with multi-purpose control. Unlike manned aviation, an unmanned aerial vehicle requires additional modules in its control system. These include the drone itself, the operator's workplace, software, data transmission lines and blocks necessary to fulfil the set flight objectives. The range of applications of unmanned aerial vehicles in the civil sector is not limited, but with the current state of the legal framework for the use of airspace, flight operations are somewhat difficult. The article formulates the main scientific position on the methodology of solving auxiliary tasks set in the work. The methodology specifies the main research stages, and it is a generalized methodological algorithm for the implementation of scientific research, which provides theoretical developments, field observations and simulation computer modelling. As a result of the study, it was found that the motion control systems of unmanned aerial vehicles are used for the process of their differentiation by the principle of complete external control, the advantages of which are considered in the work. For external control of divergence process of unmanned aerial vehicles, a method is considered for assessing the situation of convergence of unmanned aerial vehicles and choosing the manoeuvre of their difference using the area of dangerous courses, unmanned aerial vehicles approach, and it is possible to take into account the inertia of unmanned aerial vehicles when turning and the presence of navigational hazards that are in the manoeuvring area.
三架无人机的飞行控制与避碰
无人机是一种具有多用途控制的硬件和软件综合体。与有人驾驶飞机不同,无人驾驶飞行器在其控制系统中需要额外的模块。这些包括无人机本身、操作员的工作场所、软件、数据传输线和实现设定飞行目标所需的模块。无人机在民用领域的应用范围不受限制,但以目前使用空域的法律框架状况,飞行作业有些困难。本文阐述了解决工作中设置的辅助任务的方法的主要科学立场。该方法规定了主要的研究阶段,是一种用于实施科学研究的广义方法算法,提供了理论发展、实地观测和模拟计算机建模。通过研究发现,无人机运动控制系统是采用完全外部控制原理对其进行微分的过程,在工作中考虑了其优点。针对无人机发散过程的外部控制,考虑了一种利用危险航道区域、无人机进近来评估无人机收敛情况并选择其差异机动的方法,该方法可以考虑无人机转向时的惯性以及机动区域内存在的航行危险。
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
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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