一种新的对抗性攻击的鲁棒支持向量回归飞行动力学建模方法

IF 0.3 Q4 ENGINEERING, AEROSPACE SAE International Journal of Aerospace Pub Date : 2023-03-24 DOI:10.4271/01-16-03-0019
S. Hashemi, R. Botez
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引用次数: 3

摘要

精确的无人机飞行动力学模型(FDM)使我们能够在早期开发阶段设计其高效的控制器,并在降低成本的同时提高安全性。飞行测试通常针对预先确定的许多飞行条件进行,然后使用数学方法来获得整个飞行包线的FDM。对于我们的UAS-S4 Ehecatl,使用了216个对应于不同飞行条件的本地FDM来创建其本地线性计划飞行动力学模型(LLS-FDM)。使用插值和外插方法进一步增强了包含216个局部FDM的初始飞行包线数据,从而将修剪后的局部FDM数量增加到3642个。基于这个增强的数据集,支持向量机(SVM)方法被用作基准回归算法,因为它在训练样本不能线性分离时具有优异的性能。经过训练的支持向量回归(SVR)预测了整个飞行包线的FDM。尽管SVR-FDM表现出了出色的性能,但它仍然容易受到对抗性攻击。因此,我们使用对抗性再训练防御算法对其进行了修改,将其转换为鲁棒SVR-FDM。对于验证研究,基于根轨迹图评估预测的UAS-S4 FDM的质量。预测的特征值与原始特征值的接近性证实了UAS-S4 SVR-FDM的高精度。在216种飞行条件下,针对不同数量的邻居,评估了SVR预测精度,并考虑了各种核函数。此外,基于闭环控制结构中状态变量的阶跃响应,分析了回归性能。SVR-FDM提供了最短的上升时间和稳定时间,但当对SVR施加对抗性攻击时,它失败了。鲁棒SVR-FDM阶跃响应特性表明,它可以提供比LLS-FDM方法更准确的结果,同时保护控制器免受对抗性攻击。
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A Novel Flight Dynamics Modeling Using Robust Support Vector Regression against Adversarial Attacks
An accurate Unmanned Aerial System (UAS) Flight Dynamics Model (FDM) allows us to design its efficient controller in early development phases and to increase safety while reducing costs. Flight tests are normally conducted for a pre-established number of flight conditions, and then mathematical methods are used to obtain the FDM for the entire flight envelope. For our UAS-S4 Ehecatl, 216 local FDMs corresponding to different flight conditions were utilized to create its Local Linear Scheduled Flight Dynamics Model (LLS-FDM). The initial flight envelope data containing 216 local FDMs was further augmented using interpolation and extrapolation methodologies, thus increasing the number of trimmed local FDMs of up to 3,642. Relying on this augmented dataset, the Support Vector Machine (SVM) methodology was used as a benchmarking regression algorithm due to its excellent performance when training samples could not be separated linearly. The trained Support Vector Regression (SVR) predicted the FDM for the entire flight envelope. Although the SVR-FDM showed excellent performance, it remained vulnerable to adversarial attacks. Hence, we modified it using an adversarial retraining defense algorithm by transforming it into a Robust SVR-FDM. For validation studies, the quality of predicted UAS-S4 FDM was evaluated based on the Root Locus diagram. The closeness of predicted eigenvalues to the original eigenvalues confirmed the high accuracy of the UAS-S4 SVR-FDM. The SVR prediction accuracy was evaluated at 216 flight conditions, for different numbers of neighbors, and a variety of kernel functions were also considered. In addition, the regression performance was analyzed based on the step response of state variables in the closed-loop control architecture. The SVR-FDM provided the shortest rise time and settling time, but it failed when adversarial attacks were imposed on the SVR. The Robust-SVR-FDM step response properties showed that it could provide more accurate results than the LLS-FDM approach while protecting the controller from adversarial attacks.
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来源期刊
SAE International Journal of Aerospace
SAE International Journal of Aerospace ENGINEERING, AEROSPACE-
CiteScore
0.70
自引率
0.00%
发文量
22
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