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Piece-wise Identification and Analysis of the Aerodynamic Coefficients, Trim Conditions, and Safe Sets of the Generic Transport Model

机译:通用运输模型的空气动力学系数,修整条件和安全集的分段识别和分析

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Aeronautical research has investigated the Generic Transport Model (GTM) in wind-tunnel studies and provides today an elaborated aerodynamic model for designing methods dedicated to convergence analysis or control problems of aerial vehicles. In this paper, we propose a novel approach for fitting aerodynamic coefficients, namely piece-wise polynomial identification, which is based on measurements in both pre- and post-stall region. The developed method suggests a systematic approach to determine full envelope better than the purely polynomial models published yet. As a result, an analysis of GTM's longitudinal trim conditions has been successfully applied on the piece-wise identified model and achieves better results than polynomial models. Based on the trim conditions, safe set computation for linear-quadratic controllers is argued to be a powerful tool for verification of nonlinear control systems. Using common and multiple Lyapunov-functions theory, we are able to present a method for the safe set computation with piece-wise defined systems dynamics.
机译:航空研究已经在风洞研究中研究了通用运输模型(GTM),并且今天为设计用于航空器收敛性分析或控制问题的方法提供了详细的空气动力学模型。在本文中,我们提出了一种新的拟合空气动力学系数的方法,即分段多项式识别,该方法基于失速前后区域的测量。与尚未发布的纯多项式模型相比,已开发的方法提出了一种更好地确定全包络的系统方法。结果,对GTM的纵向修剪条件的分析已成功地应用于分段识别的模型,并且比多项式模型获得了更好的结果。基于微调条件,线性二次控制器的安全设置计算被认为是验证非线性控制系统的有力工具。使用通用和多重Lyapunov函数理论,我们能够提出一种使用分段定义的系统动力学进行安全集合计算的方法。

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