METHOD OF IMPROVING THE ACCURACY OF NAVIGATION MEMS DATA PROCESSING OF UAV INERTIAL NAVIGATION SYSTEM

IF 0.2 Q4 COMPUTER SCIENCE, HARDWARE & ARCHITECTURE Radio Electronics Computer Science Control Pub Date : 2022-10-18 DOI:10.15588/1607-3274-2022-3-18
O. Fesenko, R. Bieliakov, H. Radzivilov, S. A. Sasin, O. V. Borysov, I. V. Borysov, T. M. Derkach, O. O. Kovalchuk
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Abstract

Context. Modern theory and practice of preparation and conduct of hostilities on land, at sea, in the air, and recently in cyberspace dictates the relentless modernization of military equipment. The development of fundamentally new weapons is carried out considering one of the main requirements – maximum automation of operational processes, which allows combatants to distance themselves from each other as much as possible. Among the newest models of armaments on the battlefield, due to the predominantly positional nature of the armed confrontation, unmanned aerial vehicles (UAVs) have become virtually indispensable due to their own multitasking. One of the ways to increase the efficiency of UAVs on the battlefield is to increase the level of technical perfection of flight control systems. Creating new approaches to the design of unmanned aerial vehicle navigation systems, in particular, based on a platformless inertial navigation system is an urgent task that will provide automatic control of the UAV flight route in the absence of corrective signals from the global satellite navigation system. Objective. The purpose of this work is to develop a method for improving the accuracy of MEMC navigation data processing of an inertial navigation system of an unmanned aerial vehicle based on an advanced Madgwik filter. This method will increase the speed of data processing of navigation parameters and the accuracy of determining the positioning parameters in the space of the UAV through the use of an advanced Madgwik filter. The paper shows the developed block diagram of MEMS PINS filtration on the basis of the improved Madgwik filter, the detailed mathematical description of filtration processes is carried out. This method was tested experimentally in the MATLAB software environment using a real set of data collected during the flight of the UAV. Method. To achieve this goal, the following methods were used: intelligent systems, theory of automatic control, pseudo-spectral method; methods based on genetic algorithm and fuzzy neural network apparatus. Results. A method for improving the accuracy of MEMC navigation data processing of an inertial navigation system of an unmanned aerial vehicle based on an advanced Madgwik filter has been developed. The possibility of practical application of the obtained results and in comparison, with traditional methods is investigated. An experiment was performed in the MatLab software environment, and a comparison was made with the method of processing navigation data based on the Madgwik filter and the Kalman filter. Conclusions. The developed method of increasing the accuracy of MEMC navigation data processing of an inertial navigation system of an unmanned aerial vehicle based on an advanced Madgwik filter shows an advantage over known methods in the absence of corrective signals from the global satellite navigation system for accuracy and speed of navigation data processing.
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提高无人机惯导系统导航微机电系统数据处理精度的方法
上下文。在陆地、海上、空中以及最近在网络空间准备和实施敌对行动的现代理论和实践,决定了军事装备的无情现代化。从根本上说,新武器的发展是考虑到一个主要要求-最大限度地实现作战过程的自动化,这使得战斗人员尽可能地彼此保持距离。在战场上的最新武器型号中,由于武装对抗的主要位置性质,无人驾驶飞行器(uav)由于其自身的多任务处理而几乎不可或缺。提高无人机在战场上的作战效率的途径之一是提高飞控系统的技术完善水平。创建无人机导航系统设计的新方法,特别是基于无平台惯性导航系统,是一项紧迫的任务,它将在缺乏全球卫星导航系统校正信号的情况下提供无人机飞行路线的自动控制。目标。本研究的目的是开发一种基于先进Madgwik滤波器的无人机惯性导航系统MEMC导航数据处理精度的方法。该方法将通过使用先进的Madgwik滤波器,提高导航参数的数据处理速度和确定无人机空间定位参数的精度。本文给出了基于改进Madgwik滤波器的MEMS PINS滤波框图,并对滤波过程进行了详细的数学描述。利用无人机飞行过程中采集的一组真实数据,在MATLAB软件环境下对该方法进行了实验验证。方法。为了实现这一目标,采用了以下方法:智能系统、自动控制理论、伪谱法;方法基于遗传算法和模糊神经网络装置。结果。提出了一种基于Madgwik滤波器的无人机惯性导航系统MEMC导航数据处理精度提高方法。研究了所得结果的实际应用可能性,并与传统方法进行了比较。在MatLab软件环境下进行了实验,并与基于Madgwik滤波和卡尔曼滤波的导航数据处理方法进行了比较。结论。开发的基于先进Madgwik滤波器的无人机惯性导航系统MEMC导航数据处理精度提高方法,在没有来自全球卫星导航系统的校正信号的情况下,具有导航数据处理精度和速度的优势。
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来源期刊
Radio Electronics Computer Science Control
Radio Electronics Computer Science Control COMPUTER SCIENCE, HARDWARE & ARCHITECTURE-
自引率
20.00%
发文量
66
审稿时长
12 weeks
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