DYNAMICS OF CIRCULAR THIN MEMBRANE SOLAR ARRAYS BASED ON GROUND ZERO-GRAVITY SIMULATION TEST

Yunfei Yang; Litong Wang; Yanfang Liu; Shuanli Jia

doi:10.1049/ICP.2022.1925

DYNAMICS OF CIRCULAR THIN MEMBRANE SOLAR ARRAYS BASED ON GROUND ZERO-GRAVITY SIMULATION TEST

Yunfei Yang
, Litong Wang
, Yanfang Liu^*
, Shuanli Jia

^*Corresponding author for this work

School of Astronautics

Harbin Institute of Technology
Tianjin Aerospace Electromechanical Equipment Research Institute

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

3 Scopus citations

Abstract

Our country's asteroid prober will use circular thin membrane solar arrays, which is the first time for China to use this technology. In this paper, the dynamics of the deployment of the circular thin-film solar arrays in space and under the simulated zero-gravity environment are compared. Firstly, the kinematics and dynamics of the circular solar thin-film arrays in zero gravity and low gravity environment are analyzed based on ADAMS. Results indicate the importance of gravity compensation accuracy in the ground experiment. This step is necessary as a reference for subsequent analysis. Besides, the zero-gravity compensation system is designed carefully for the circular solar arrays, which mainly uses the passive support method based on the air-pad to compensate for the gravity of the solar arrays. The normal deployment of the solar arrays will certainly be affected by the disturbing force generated by the zero-gravity test system. These effects are measured experimentally and introduced into ADMAS. A comparison of the kinematics & dynamics of the circular thin-film solar arrays between the real and the simulated zero-gravity environments shows the feasibility and limitations of this zero-gravity compensation system, which can guide engineering practice.

Original language	English
Title of host publication	IET Conference Proceedings
Publisher	Institution of Engineering and Technology
Pages	847-851
Number of pages	5
Volume	2022
Edition	13
ISBN (Electronic)	9781839537837
DOIs	https://doi.org/10.1049/ICP.2022.1925
State	Published - 2022
Event	1st International Conference on Mechanical System Dynamics, ICMSD 2022 - Nanjing, China Duration: 24 Aug 2022 → 27 Aug 2022

Conference

Conference	1st International Conference on Mechanical System Dynamics, ICMSD 2022
Country/Territory	China
City	Nanjing
Period	24/08/22 → 27/08/22

Keywords

GROUND ZERO-GRAVITY TEST
KINEMATICS AND DYNAMICS
THE CIRCULAR THIN MEMBRANE SOLAR ARRAYS

Access to Document

10.1049/ICP.2022.1925

Cite this

@inproceedings{735160928ff74fa59c542cca8ac199d7,

title = "DYNAMICS OF CIRCULAR THIN MEMBRANE SOLAR ARRAYS BASED ON GROUND ZERO-GRAVITY SIMULATION TEST",

abstract = "Our country's asteroid prober will use circular thin membrane solar arrays, which is the first time for China to use this technology. In this paper, the dynamics of the deployment of the circular thin-film solar arrays in space and under the simulated zero-gravity environment are compared. Firstly, the kinematics and dynamics of the circular solar thin-film arrays in zero gravity and low gravity environment are analyzed based on ADAMS. Results indicate the importance of gravity compensation accuracy in the ground experiment. This step is necessary as a reference for subsequent analysis. Besides, the zero-gravity compensation system is designed carefully for the circular solar arrays, which mainly uses the passive support method based on the air-pad to compensate for the gravity of the solar arrays. The normal deployment of the solar arrays will certainly be affected by the disturbing force generated by the zero-gravity test system. These effects are measured experimentally and introduced into ADMAS. A comparison of the kinematics \& dynamics of the circular thin-film solar arrays between the real and the simulated zero-gravity environments shows the feasibility and limitations of this zero-gravity compensation system, which can guide engineering practice.",

keywords = "GROUND ZERO-GRAVITY TEST, KINEMATICS AND DYNAMICS, THE CIRCULAR THIN MEMBRANE SOLAR ARRAYS",

author = "Yunfei Yang and Litong Wang and Yanfang Liu and Shuanli Jia",

note = "Publisher Copyright: {\textcopyright} 2022 IET Conference Proceedings. All rights reserved.; 1st International Conference on Mechanical System Dynamics, ICMSD 2022 ; Conference date: 24-08-2022 Through 27-08-2022",

year = "2022",

doi = "10.1049/ICP.2022.1925",

language = "英语",

volume = "2022",

pages = "847--851",

booktitle = "IET Conference Proceedings",

publisher = "Institution of Engineering and Technology",

address = "英国",

edition = "13",

}

Yang, Y, Wang, L, Liu, Y & Jia, S 2022, DYNAMICS OF CIRCULAR THIN MEMBRANE SOLAR ARRAYS BASED ON GROUND ZERO-GRAVITY SIMULATION TEST. in IET Conference Proceedings. 13 edn, vol. 2022, Institution of Engineering and Technology, pp. 847-851, 1st International Conference on Mechanical System Dynamics, ICMSD 2022, Nanjing, China, 24/08/22. https://doi.org/10.1049/ICP.2022.1925

TY - GEN

T1 - DYNAMICS OF CIRCULAR THIN MEMBRANE SOLAR ARRAYS BASED ON GROUND ZERO-GRAVITY SIMULATION TEST

AU - Yang, Yunfei

AU - Wang, Litong

AU - Liu, Yanfang

AU - Jia, Shuanli

PY - 2022

Y1 - 2022

N2 - Our country's asteroid prober will use circular thin membrane solar arrays, which is the first time for China to use this technology. In this paper, the dynamics of the deployment of the circular thin-film solar arrays in space and under the simulated zero-gravity environment are compared. Firstly, the kinematics and dynamics of the circular solar thin-film arrays in zero gravity and low gravity environment are analyzed based on ADAMS. Results indicate the importance of gravity compensation accuracy in the ground experiment. This step is necessary as a reference for subsequent analysis. Besides, the zero-gravity compensation system is designed carefully for the circular solar arrays, which mainly uses the passive support method based on the air-pad to compensate for the gravity of the solar arrays. The normal deployment of the solar arrays will certainly be affected by the disturbing force generated by the zero-gravity test system. These effects are measured experimentally and introduced into ADMAS. A comparison of the kinematics & dynamics of the circular thin-film solar arrays between the real and the simulated zero-gravity environments shows the feasibility and limitations of this zero-gravity compensation system, which can guide engineering practice.

AB - Our country's asteroid prober will use circular thin membrane solar arrays, which is the first time for China to use this technology. In this paper, the dynamics of the deployment of the circular thin-film solar arrays in space and under the simulated zero-gravity environment are compared. Firstly, the kinematics and dynamics of the circular solar thin-film arrays in zero gravity and low gravity environment are analyzed based on ADAMS. Results indicate the importance of gravity compensation accuracy in the ground experiment. This step is necessary as a reference for subsequent analysis. Besides, the zero-gravity compensation system is designed carefully for the circular solar arrays, which mainly uses the passive support method based on the air-pad to compensate for the gravity of the solar arrays. The normal deployment of the solar arrays will certainly be affected by the disturbing force generated by the zero-gravity test system. These effects are measured experimentally and introduced into ADMAS. A comparison of the kinematics & dynamics of the circular thin-film solar arrays between the real and the simulated zero-gravity environments shows the feasibility and limitations of this zero-gravity compensation system, which can guide engineering practice.

KW - GROUND ZERO-GRAVITY TEST

KW - KINEMATICS AND DYNAMICS

KW - THE CIRCULAR THIN MEMBRANE SOLAR ARRAYS

UR - https://www.scopus.com/pages/publications/85174646694

U2 - 10.1049/ICP.2022.1925

DO - 10.1049/ICP.2022.1925

M3 - 会议稿件

AN - SCOPUS:85174646694

VL - 2022

SP - 847

EP - 851

BT - IET Conference Proceedings

PB - Institution of Engineering and Technology

T2 - 1st International Conference on Mechanical System Dynamics, ICMSD 2022

Y2 - 24 August 2022 through 27 August 2022

ER -

DYNAMICS OF CIRCULAR THIN MEMBRANE SOLAR ARRAYS BASED ON GROUND ZERO-GRAVITY SIMULATION TEST

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