Modal Parameter Identification of the New Type of Airship with Multi-Airbag Hybrid Configuration Based on the Stochastic Subspace Method

The new type of multi-airbag hybrid airship is a novel lighter-than-air platform, but its flexible structures pose challenges for accurate modal parameter identification under complex fluid-structure interaction. Traditional methods often fail to capture the dynamic characteristics of such compliant systems. In this paper, a stochastic subspace identification method is proposed to estimate the modal parameters of the three capsule hybrid airship. The method constructs the Hankel matrix using only output response data and extracts the system matrix by singular value decomposition so as to identify the natural frequency and damping coefficient. Moreover, the numerical model of the airship (aspect ratio 2.22) is built, and the simulated response data (first five modes) are used to validate the approach. The results show that the identified frequencies and damping ratios match the theoretical values with a maximum error of 6.35%, demonstrating good accuracy and robustness. The proposed technique can provide a reliable tool for online modal identification of flexible airships, supporting structural health monitoring and vibration control.

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Publication Details

Journal
Aerospace
Published
2026-07-02
DOI
https://doi.org/10.3390/aerospace13070609
Primary Topic
Aerospace Engineering and Energy Systems
Type
article
Field-Weighted Citation Impact
0.00

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Modal Parameter Identification of the New Type of Airship with Multi-Airbag Hybrid Configuration Based on the Stochastic Subspace Method

Xicheng Zhang, Longbin Liu, Xiaolu Hu, Mengyang Fan
Aerospace
Aerospace Engineering and Energy Systems
article

Modal Parameter Identification of the New Type of Airship with Multi-Airbag Hybrid Configuration Based on the Stochastic Subspace Method

Xicheng Zhang, Longbin Liu, Xiaolu Hu, Mengyang Fan
article en

Abstract

The new type of multi-airbag hybrid airship is a novel lighter-than-air platform, but its flexible structures pose challenges for accurate modal parameter identification under complex fluid-structure interaction. Traditional methods often fail to capture the dynamic characteristics of such compliant systems. In this paper, a stochastic subspace identification method is proposed to estimate the modal parameters of the three capsule hybrid airship. The method constructs the Hankel matrix using only output response data and extracts the system matrix by singular value decomposition so as to identify the natural frequency and damping coefficient. Moreover, the numerical model of the airship (aspect ratio 2.22) is built, and the simulated response data (first five modes) are used to validate the approach. The results show that the identified frequencies and damping ratios match the theoretical values with a maximum error of 6.35%, demonstrating good accuracy and robustness. The proposed technique can provide a reliable tool for online modal identification of flexible airships, supporting structural health monitoring and vibration control.

AerospaceVol. 13(7)
National University of Defense Technology (CN)
National Natural Science Foundation of China
Openalex Percentile: Top 4%
Aerospace Engineering and Energy Systems
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