Robust modal damping control for active flutter suppression

J Theis, H Pfifer, P Seiler - Journal of Guidance, Control, and Dynamics, 2020 - arc.aiaa.org
Flutter is an unstable oscillation caused by the interaction of aerodynamics and structural
dynamics. It is current practice to operate aircraft well below their open-loop flutter speed in …

[PDF][PDF] 一种新的基于LSTM 的航位推算算法

涂杰, 黎杰, 刘凯 - 舰船电子工程, 2023 - jc.journal.cssc709.net
摘要针对传统航位推算(DR) 算法中构建的运动模型简化程度较高, 对运动信息的预测精度有限,
制约DR 算法性能的问题, 提出一种新的基于长短时记忆网络(Long Short Term Memory …

[PDF][PDF] 基于改进涡格法的飞翼飞行器动力学建模方法

郑维新, 刘海颖 - 舰船电子工程, 2023 - jc.journal.cssc709.net
摘要针对柔性飞翼飞行器动力学建模中存在的气动非线性问题, 提出了一种基于改进涡格法的非
线性动力学飞翼飞行器建模方法. 首先, 对飞翼飞行器的几何参数和结构特性进行了介绍和分析 …

System identification in time domain of flexible aircraft using panel methods

TR de Paula, AGP Sarmento… - Journal of Physics …, 2024 - iopscience.iop.org
The motivation to accurately model the dynamics of flexible aircraft grew with the
development of energy-efficient aircraft, consequently, great aspect ratio aircraft. The …