Technical Papers
Jan 31, 2024

Experimental Investigation of Deployment Process of Large Hoop Truss Antenna for Space

Publication: Journal of Aerospace Engineering
Volume 37, Issue 3

Abstract

Large hoop truss antennas are locked into a stable structure during deployment in space. The key to characterizing the performance of each mechanism, and discovering problems in the deployment process, is the three-dimensional motion of the antenna. Therefore, it is important to measure antenna motion with high precision for antenna design. Contact measurement requires sensors to be attached to the object, affecting the motion of the antenna; thus, noncontact measurement is the preferred measurement method. For a large antenna, a large field of view and observation angle are required to measure the deployment process. Traditional binocular stereo vision measurement is not sufficiently accurate. In this paper, 36 cameras were combined into an array to measure antenna deployment. A high-precision triggering system was designed, a calibration method suitable for large-scale, multiangle measurement was developed, and a reconstruction method based on the geometric constraints was proposed, greatly improving measurement resolution. The camera array was used to measure the motion of a large hoop truss antenna with a diameter of 4 m during deployment. Based on the measured parameters, the angular velocity of each antenna mechanism was calculated, and the synchronization of the antenna structure was analyzed.

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Data Availability Statement

Some or all data, models, or code generated or used during the study are proprietary or confidential in nature and may only be provided with restrictions.

Acknowledgments

This work was supported by the National Natural Science Foundation of China (Grant Nos. 11772053 and 11727801). Thank you for the help by Prof. Qiang Tian in the analysis and experimental study of antenna dynamic behavior during this research work.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 3May 2024

History

Received: Mar 19, 2023
Accepted: Sep 21, 2023
Published online: Jan 31, 2024
Published in print: May 1, 2024
Discussion open until: Jun 30, 2024

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Dept. of Mechanics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, PR China. Email: [email protected]
Chao Wang, Ph.D.
Dept. of Mechanics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, PR China.
Associate Professor, Dept. of Mechanics, School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, PR China (corresponding author). ORCID: https://orcid.org/0000-0003-2792-8389. Email: [email protected]

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