An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode
The axial deployment force is an indispensable parameter of a lanyard-deployed coilable mast, which reflects its load capacity in practical applications. However, research on the axial deployment force in the literature is very limited, and there are no mature numerical methods to determine this par...
Saved in:
| Main Authors: | , , , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2024-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2024/3503468 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832559651801006080 |
|---|---|
| author | Yu Liu Liang Sun Hai Huang Xurui Zhao Jiahao Liu Yishi Qiao |
| author_facet | Yu Liu Liang Sun Hai Huang Xurui Zhao Jiahao Liu Yishi Qiao |
| author_sort | Yu Liu |
| collection | DOAJ |
| description | The axial deployment force is an indispensable parameter of a lanyard-deployed coilable mast, which reflects its load capacity in practical applications. However, research on the axial deployment force in the literature is very limited, and there are no mature numerical methods to determine this parameter in the design stage of coilable masts. In this paper, a numerical method for determining the axial deployment force of a lanyard-deployed coilable mast in the local coil mode is presented. Through this method, the designer can quickly obtain the estimated value of the axial deployment force in the design stage, which is convenient for the quantitative design of parameters. To verify the correctness of the proposed method, a dynamic simulation of the coilable mast is carried out, and a microgravity test is performed. The comparison results show that the error between the numerical method and the simulation and experimental results is less than 5%, which proves the correctness of the proposed method. In addition, the coilable mast studied in this paper has been verified by an actual microsatellite deployment in orbit. |
| format | Article |
| id | doaj-art-c14bf047646e4164917dbd99c8d7988b |
| institution | Kabale University |
| issn | 1687-5974 |
| language | English |
| publishDate | 2024-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-c14bf047646e4164917dbd99c8d7988b2025-02-03T01:29:35ZengWileyInternational Journal of Aerospace Engineering1687-59742024-01-01202410.1155/2024/3503468An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil ModeYu Liu0Liang Sun1Hai Huang2Xurui Zhao3Jiahao Liu4Yishi Qiao5School of AstronauticsSchool of AstronauticsSchool of AstronauticsInstitute of Remote Sensing SatelliteSchool of AstronauticsSatellite Engineering DepartmentThe axial deployment force is an indispensable parameter of a lanyard-deployed coilable mast, which reflects its load capacity in practical applications. However, research on the axial deployment force in the literature is very limited, and there are no mature numerical methods to determine this parameter in the design stage of coilable masts. In this paper, a numerical method for determining the axial deployment force of a lanyard-deployed coilable mast in the local coil mode is presented. Through this method, the designer can quickly obtain the estimated value of the axial deployment force in the design stage, which is convenient for the quantitative design of parameters. To verify the correctness of the proposed method, a dynamic simulation of the coilable mast is carried out, and a microgravity test is performed. The comparison results show that the error between the numerical method and the simulation and experimental results is less than 5%, which proves the correctness of the proposed method. In addition, the coilable mast studied in this paper has been verified by an actual microsatellite deployment in orbit.http://dx.doi.org/10.1155/2024/3503468 |
| spellingShingle | Yu Liu Liang Sun Hai Huang Xurui Zhao Jiahao Liu Yishi Qiao An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode International Journal of Aerospace Engineering |
| title | An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode |
| title_full | An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode |
| title_fullStr | An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode |
| title_full_unstemmed | An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode |
| title_short | An Iterative Determination Method of an Axial Deployment Force of a Lanyard-Deployed Coilable Mast in Local Coil Mode |
| title_sort | iterative determination method of an axial deployment force of a lanyard deployed coilable mast in local coil mode |
| url | http://dx.doi.org/10.1155/2024/3503468 |
| work_keys_str_mv | AT yuliu aniterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT liangsun aniterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT haihuang aniterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT xuruizhao aniterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT jiahaoliu aniterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT yishiqiao aniterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT yuliu iterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT liangsun iterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT haihuang iterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT xuruizhao iterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT jiahaoliu iterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode AT yishiqiao iterativedeterminationmethodofanaxialdeploymentforceofalanyarddeployedcoilablemastinlocalcoilmode |