Methods for the vibration determination and parameter identification of spacecraft with flexible structures

Ivanov Danil; Meus S. V.; Ovchinnikov A. V.; Ovchinnikov M. Yu; Shestakov S. A.; Yakimov E. N.

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Methods for the vibration determination and parameter identification of spacecraft with flexible structures

机译：挠性结构航天器的振动确定和参数辨识方法

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Methods for dynamic parameters identification and vibrations estimation of large spacecraft with flexible structures are reviewed. Different approaches to the structural deviation determination and to the vibration frequency identification by processing measurements from the onboard sensors are compared. Measuring devices and sensors for the motion estimation of large nonrigid structures are reviewed.

机译：综述了具有柔性结构的大型航天器的动力学参数辨识和振动估计方法。比较了通过车载传感器的处理测量结果确定结构偏差和振动频率的不同方法。综述了用于大型非刚性结构运动估计的测量设备和传感器。

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《Journal of Computer and Systems Sciences International》 |2017年第2期|311-327|共17页
作者
Ivanov Danil; Meus S. V.; Ovchinnikov A. V.; Ovchinnikov M. Yu; Shestakov S. A.; Yakimov E. N.;
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作者单位

Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, Russian Federation;

AO Information Satellite Systems, Zheleznogorsk, Russian Federation;

AO Information Satellite Systems, Zheleznogorsk, Russian Federation;

Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, Russian Federation;

Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, Russian Federation;

AO Information Satellite Systems, Zheleznogorsk, Russian Federation;

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收录信息美国《科学引文索引》(SCI);美国《工程索引》(EI);
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正文语种 eng
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1. Modal parameter identification of flexible spacecraft using the covariance-driven stochastic subspace identification (SSI-COV) method [J] . Yong Xie, Pan Liu, Guo-Ping Cai 力学学报：英文版 . 2016,第004期

机译：使用协方差驱动的随机子空间识别（SSI-COV）方法识别挠性航天器的模态参数
2. New methodology for modal parameters identification of smart civil structures using ambient vibrations and synchrosqueezed wavelet transform [J] . Carlos A. Perez-Ramirez, Juan P. Amezquita-Sanchez, Hojjat Adeli, Engineering Applications of Artificial Intelligence . 2016,第FEBa期

机译：利用环境振动和同步小波变换的智能土木结构模态参数识别新方法
3. Vibration parameters identification in a spacecraft subjected to active vibration damping [J] . A. Skullestad, O. Hallingstad Mechatronics: The Science of Intelligent Machines . 1998,第6期

机译：主动减振的航天器振动参数识别
4. Determination of Reliable Control Parameters for Monitoring of Large Flexible Structure Using Recursive Stochastic Subspace Identification [C] . Chin-Hsiung Loh, Yi-Cheng Liu International Conference on Structural Dynamics . 2011

机译：使用递增随机子空间识别测定监测大柔性结构的可靠控制参数
5. Time-domain parameter identification of aeroelastic loads by forced-vibration method for response of flexible structures subject to transient wind. [D] . Cao, Bochao. 2012

机译：气动弹性载荷时域参数识别的强迫振动方法对柔性结构在瞬态风作用下的响应。
6. An Improved Method of Parameter Identification and Damage Detection in Beam Structures under Flexural Vibration Using Wavelet Multi-Resolution Analysis [O] . Seyed Alireza Ravanfar, Hashim Abdul Razak, Zubaidah Ismail, 2015

机译：基于小波多分辨率分析的梁结构弯曲振动参数识别与损伤识别的改进方法
7. Time-domain parameter identification of aeroelastic loads by forced-vibration method for response of flexible structures subject to transient wind [O] . Cao, Bochao 2012

机译：基于瞬态风响应的弹性振动响应的强迫振动时空参数识别
8. Approximation Methods for the Identification and Control of Distributed Parameter Systems with Applications to Flexible Structures. [R] . Rosen, I. G. 1991

机译：分布参数系统辨识与控制的近似方法及其在柔性结构中的应用。

Methods for the vibration determination and parameter identification of spacecraft with flexible structures

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