收藏切换
Time-varying modal parameter estimation of the CERES-1 launch vehicle
收藏切换
PDF
Zhi-sai MA1, 2, Qian DING1, 2, Bai-qi LIU3, Jian-she LIU3, Jun-feng ZHANG3, Wei-li DONG3
Journal of Vibration Engineering | 2024, 37(5) : 729 - 736
Less
收藏切换
Journal of Vibration Engineering | 2024, 37(5): 729-736
Time-varying modal parameter estimation of the CERES-1 launch vehicle
Full
Zhi-sai MA1, 2, Qian DING1, 2, Bai-qi LIU3, Jian-she LIU3, Jun-feng ZHANG3, Wei-li DONG3
Affiliations
  • 1School of Mechanical Engineering, Tianjin University, Tianjin 300350, China
  • 2Tianjin Key Laboratory of Nonlinear Dynamics and Control, Tianjin 300350, China
  • 3Beijing Galactic Energy Equipment Technology Co., Ltd., Beijing 100176, China
Published: 2024-05-28 doi: 10.16385/j.cnki.issn.1004-4523.2024.05.001
Outline
收藏切换

It is usually difficult to establish the dynamic model of a launch vehicle that accurately describes its time-varying characteristics. Therefore modal identification techniques are particularly necessary to obtain the time-varying dynamic characteristics of launch vehicles under flight conditions. Aiming at the problem of in-flight modal identification of launch vehicles,an output-only recursive identification method based on the time-dependent autoregressive moving average model is developed by using exponentially weighted mechanisms to track the time-varying characteristics. Without measuring the natural excitation forces,the proposed method can accurately and quickly identify the time-varying modal parameters of launch vehicles by exclusively using the measured response signals. Taking the CERES-1 launch vehicle as an example,time-varying modal parameters before liftoff and during the flight phase are accurately estimated by processing the flight telemetry data. Identification results are consistent with the variation of the finite element analysis results,demonstrating the high achievable accuracy of the proposed method. The proposed in-flight modal identification method can obtain the full-cycle modal information of launch vehicles,which meets the engineering requirements for the finite element model updating and attitude control system design.

launch vehicle  /  time-varying modal parameter  /  CERES-1  /  recursive identification
Zhi-sai MA, Qian DING, Bai-qi LIU, Jian-she LIU, Jun-feng ZHANG, Wei-li DONG. Time-varying modal parameter estimation of the CERES-1 launch vehicle[J]. Journal of Vibration Engineering, 2024 , 37 (5) : 729 -736 . DOI: 10.16385/j.cnki.issn.1004-4523.2024.05.001
Year 2024 volume 37 Issue 5
PDF
114
57
Cite this Article
BibTeX
Article Info
doi: 10.16385/j.cnki.issn.1004-4523.2024.05.001
  • Receive Date:2023-01-18
  • Online Date:2026-02-09
  • Published:2024-05-28
Article Data
Affiliations
History
  • Received:2023-01-18
  • Revised:2023-05-04
Funding
Affiliations
    1School of Mechanical Engineering, Tianjin University, Tianjin 300350, China
    2Tianjin Key Laboratory of Nonlinear Dynamics and Control, Tianjin 300350, China
    3Beijing Galactic Energy Equipment Technology Co., Ltd., Beijing 100176, China
References
Share
https://castjournals.cast.org.cn/joweb/zdgcxb/EN/10.16385/j.cnki.issn.1004-4523.2024.05.001
Share to
QR

Scan QR to access full text

Cite this article
BibTeX
Citations
表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
关闭全屏
  • BibTeX
  • EndNote
  • RefWorks
  • TxT