基于动态反演的AURORA飞艇控制系统稳定性和鲁棒性分析

Alexandra Moutinho, J. Azinheira
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引用次数: 68

摘要

本文对AURORA项目自主飞艇非线性控制系统的稳定性和鲁棒性进行了分析。利用线性最优补偿器给出的期望动态,实现了动态逆控制器。应用李雅普诺夫稳定性理论对非线性系统进行了稳定性分析。为了验证非线性控制器在面对干扰和模型参数误差时的性能,进行了鲁棒性测试。得到的结果说明了整个系统的鲁棒性,并指出了极光飞艇最敏感的模型参数,对于这些参数需要进行更仔细的识别/确定。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Stability and Robustness Analysis of the AURORA Airship Control System using Dynamic Inversion
This paper presents a stability and robustness analysis of a nonlinear control system for the autonomous airship of the AURORA project. A Dynamic Inversion controller is implemented with desired dynamics given by a linear optimal compensator. The stability analysis of the nonlinear system is done applying Lyapunov’s stability theory. Robustness tests are performed in order to verify the nonlinear controller performance in face of disturbances and model parameters errors. The results obtained illustrate the overall system robustness, and point at the most sensitive model parameters of the AURORA airship, for which a more careful identification/determination should be carried.
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