Robust Performance Analysis on Dynamic Control of Unmanned Aerial Vehicle System Using Bode Plot

Hteik Tin Cho Nyunt, Thanda Win, H. Tun
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Abstract

The paper focuses on the robust performance analysis on dynamic control of unmanned aerial vehicle system with numerical computation. The objectives of this work are to find the appropriate solution for robust stability problems for dynamic control of unmanned aerial vehicle (UAV) system which is critical challenge in the space technology. The background of the theoretical work on digital control system is very important to study the problem of dynamic control system at present. The idea behind the control system stability analysis on digital technology is very important candidate in space technology. The specific purpose on analyzing the performance of dynamic of digital control system for space technology is solved in this paper. The mathematical model of target system is mentioned and analyzed based on the classical control method with digital technology. The related work for modeling of the control system is mentioned and expressed the detailed background for the analysis. The simulation results confirm that the proposed system met the robust performance for digital control of UAV system for reality. The analysis has been carried out based on feedback control system stability for dynamic system as well. The simulation results for stability analysis have been carried out by using MATLAB programming languages.
基于波德图的无人机系统动态控制鲁棒性能分析
本文采用数值计算方法对无人机系统的动态控制进行鲁棒性分析。针对无人机系统动态控制的鲁棒稳定性问题,寻找合适的解决方案,是空间技术领域的重要挑战。数字控制系统理论研究的背景对当前动态控制系统问题的研究具有重要意义。控制系统稳定性分析背后的思想是数字技术在空间技术中非常重要的候选者。本文解决了空间技术数字控制系统动态性能分析的具体问题。在经典控制方法的基础上,利用数字技术对目标系统的数学模型进行了分析。介绍了控制系统建模的相关工作,并阐述了分析的详细背景。仿真结果表明,该系统能够满足实际无人机系统数字控制的鲁棒性要求。对动态系统进行了基于反馈控制的稳定性分析。利用MATLAB编程语言进行了稳定性分析的仿真结果。
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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