A two-stage torsion pendulum to test AC control actuator of space inertial sensor for Tianqin.
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| Title: | A two-stage torsion pendulum to test AC control actuator of space inertial sensor for Tianqin. |
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| Authors: | Jiang, Yiyan1 (AUTHOR), Lu, Jinfeng1 (AUTHOR), Ouyang, Chaoli1 (AUTHOR), Zhou, Hongtao1 (AUTHOR), Hu, Ming1 (AUTHOR), Liu, Li1 (AUTHOR), Wu, Shuchao1 (AUTHOR) scwu@hust.edu.cn, Zhou, Zebing1 (AUTHOR) zhouzb@hust.edu.cn |
| Source: | Measurement Science & Technology. Jan2026, Vol. 37 Issue 4, p1-11. 11p. |
| Subjects: | Electrostatic actuators, Inertial navigation systems, Pendulums, Sensitivity analysis, Multi-degree of freedom, Gravitational wave detectors |
| Abstract: | To realize the free falling test mass (TM) in gravitational wave detection in space, an alternative current (AC) electrostatic control strategy is proposed and developed. It is significant to test and verify the AC control actuation scheme on the ground. In this paper, a two-stage torsion pendulum is used to test the performance of the AC control actuator of inertial sensor for Tianqin project. First, the pendulum facility combined with a TM, a capacitive position sensor and an AC control actuator is constructed. Experimental results show that the sensitivities of the pendulum achieve 4.2 × 10−11 N Hz−1/2 at 6 mHz and 1.6 × 10−13 Nm Hz−1/2 at 15 mHz, respectively, and the pendulum provides a chance to realize the performance test of two degree-of-freedom sensitivities of the actuator, experimental verification of AC control strategy and so on, which is first reported to test performance of the AC control actuator of a space inertial sensor on the ground. [ABSTRACT FROM AUTHOR] |
| Copyright of Measurement Science & Technology is the property of IOP Publishing and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.) | |
| Database: | Engineering Source |
| FullText | Text: Availability: 0 |
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| Header | DbId: egs DbLabel: Engineering Source An: 190858038 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: A two-stage torsion pendulum to test AC control actuator of space inertial sensor for Tianqin. – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Jiang%2C+Yiyan%22">Jiang, Yiyan</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Lu%2C+Jinfeng%22">Lu, Jinfeng</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Ouyang%2C+Chaoli%22">Ouyang, Chaoli</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Zhou%2C+Hongtao%22">Zhou, Hongtao</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Hu%2C+Ming%22">Hu, Ming</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Liu%2C+Li%22">Liu, Li</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Wu%2C+Shuchao%22">Wu, Shuchao</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> scwu@hust.edu.cn</i><br /><searchLink fieldCode="AR" term="%22Zhou%2C+Zebing%22">Zhou, Zebing</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> zhouzb@hust.edu.cn</i> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22Measurement+Science+%26+Technology%22">Measurement Science & Technology</searchLink>. Jan2026, Vol. 37 Issue 4, p1-11. 11p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Electrostatic+actuators%22">Electrostatic actuators</searchLink><br /><searchLink fieldCode="DE" term="%22Inertial+navigation+systems%22">Inertial navigation systems</searchLink><br /><searchLink fieldCode="DE" term="%22Pendulums%22">Pendulums</searchLink><br /><searchLink fieldCode="DE" term="%22Sensitivity+analysis%22">Sensitivity analysis</searchLink><br /><searchLink fieldCode="DE" term="%22Multi-degree+of+freedom%22">Multi-degree of freedom</searchLink><br /><searchLink fieldCode="DE" term="%22Gravitational+wave+detectors%22">Gravitational wave detectors</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: To realize the free falling test mass (TM) in gravitational wave detection in space, an alternative current (AC) electrostatic control strategy is proposed and developed. It is significant to test and verify the AC control actuation scheme on the ground. In this paper, a two-stage torsion pendulum is used to test the performance of the AC control actuator of inertial sensor for Tianqin project. First, the pendulum facility combined with a TM, a capacitive position sensor and an AC control actuator is constructed. Experimental results show that the sensitivities of the pendulum achieve 4.2 × 10−11 N Hz−1/2 at 6 mHz and 1.6 × 10−13 Nm Hz−1/2 at 15 mHz, respectively, and the pendulum provides a chance to realize the performance test of two degree-of-freedom sensitivities of the actuator, experimental verification of AC control strategy and so on, which is first reported to test performance of the AC control actuator of a space inertial sensor on the ground. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of Measurement Science & Technology is the property of IOP Publishing and its content may not be copied or emailed to multiple sites without the copyright holder's express written permission. Additionally, content may not be used with any artificial intelligence tools or machine learning technologies. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract.</i> (Copyright applies to all Abstracts.) |
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| RecordInfo | BibRecord: BibEntity: Identifiers: – Type: doi Value: 10.1088/1361-6501/ae2b29 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 11 StartPage: 1 Subjects: – SubjectFull: Electrostatic actuators Type: general – SubjectFull: Inertial navigation systems Type: general – SubjectFull: Pendulums Type: general – SubjectFull: Sensitivity analysis Type: general – SubjectFull: Multi-degree of freedom Type: general – SubjectFull: Gravitational wave detectors Type: general Titles: – TitleFull: A two-stage torsion pendulum to test AC control actuator of space inertial sensor for Tianqin. Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Jiang, Yiyan – PersonEntity: Name: NameFull: Lu, Jinfeng – PersonEntity: Name: NameFull: Ouyang, Chaoli – PersonEntity: Name: NameFull: Zhou, Hongtao – PersonEntity: Name: NameFull: Hu, Ming – PersonEntity: Name: NameFull: Liu, Li – PersonEntity: Name: NameFull: Wu, Shuchao – PersonEntity: Name: NameFull: Zhou, Zebing IsPartOfRelationships: – BibEntity: Dates: – D: 30 M: 01 Text: Jan2026 Type: published Y: 2026 Identifiers: – Type: issn-print Value: 09570233 Numbering: – Type: volume Value: 37 – Type: issue Value: 4 Titles: – TitleFull: Measurement Science & Technology Type: main |
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