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细长体飞行器气动伺服弹性稳定性分析对比研究
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作者 严晓雪 许云涛 李长文 《战术导弹技术》 北大核心 2024年第3期11-16,共6页
为有效避免飞行器设计过程中面临的非定常气动力、机体结构及控制系统耦合引发的闭环系统失稳问题,针对细长体飞行器气动伺服弹性稳定性分析需求,建立了基于气动导数法与工程面元法的气动伺服弹性稳定性分析手段,对比了不同方法气动伺... 为有效避免飞行器设计过程中面临的非定常气动力、机体结构及控制系统耦合引发的闭环系统失稳问题,针对细长体飞行器气动伺服弹性稳定性分析需求,建立了基于气动导数法与工程面元法的气动伺服弹性稳定性分析手段,对比了不同方法气动伺服弹性稳定性分析的适用性。针对某细长体飞行器的研究发现,亚声速和超声速状态两种方法计算偏差在2 dB以内,偏差较小,使用两种方法评估均可;高超声速状态两种方法偏差达到10 dB,此时建议采用精度更高的气动导数法。 展开更多
关键词 细长体飞行器 气动伺服弹性 稳定性 气动导数法 工程面元 亚声速 高超声速
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Self-contained eigenvector algorithm applied to the identification of aerodynamic derivatives of bridge model 被引量:3
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作者 ZHANG XiaoXu CHEN LiFen SONG HanWen 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第5期1134-1140,共7页
On one hand, when the bridge stays in a windy environment, the aerodynamic power would reduce it to act as a non-classic system. Consequently, the transposition of the system’s right eigenmatrix will not equal its le... On one hand, when the bridge stays in a windy environment, the aerodynamic power would reduce it to act as a non-classic system. Consequently, the transposition of the system’s right eigenmatrix will not equal its left eigenmatrix any longer. On the other hand, eigenmatrix plays an important role in model identification, which is the basis of the identification of aerodynamic derivatives. In this study, we follow Scanlan’s simple bridge model and utilize the information provided by the left and right eigenmatrixes to structure a self-contained eigenvector algorithm in the frequency domain. For the purpose of fitting more accurate transfer function, the study adopts the combined sine-wave stimulation method in the numerical simulation. And from the simulation results, we can conclude that the derivatives identified by the self-contained eigenvector algorithm are more dependable. 展开更多
关键词 bridge model aerodynamic derivatives eigenvector modal analysis parameter identification
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