Exploring In‐Orbit Operations: Assessing Performance and Fault Management of the Student Small Satellite‐1 (SSS‐1).
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| Title: | Exploring In‐Orbit Operations: Assessing Performance and Fault Management of the Student Small Satellite‐1 (SSS‐1). |
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| Authors: | Liu, Bohan1,2 (AUTHOR), Li, Jia1 (AUTHOR), Niu, Xiaojie1 (AUTHOR), Liu, Yu1 (AUTHOR), Huang, Hai1 (AUTHOR) hhuang@buaa.edu.cn, Sun, Liang1 (AUTHOR), Habib, Mohammad Rezwan (AUTHOR) mohabib@wiley.com |
| Source: | International Journal of Aerospace Engineering. 6/16/2025, Vol. 2025, p1-18. 18p. |
| Subjects: | Microspacecraft, Space exploration, Astronautics, Propulsion systems, Technological innovations |
| Abstract: | Small satellites represent a pivotal advancement in space technology, offering versatile platforms for conducting educational missions with reduced costs. Initiated by the Asia‐Pacific Space Cooperation Organization (APSCO), the Student Small Satellite‐1 (SSS‐1) mission exemplifies this paradigm. SSS‐1 is designed to validate the deployment of the coilable mast and conduct diverse space experiments in orbit. This paper provides a detailed exploration of the SSS‐1 space experiments and the fault handling procedures. Firstly, the overview of SSS‐1 is presented in this paper. Next, it details the results of various space experiments, including space imaging, remote sensing, electrical propulsion system tests, and Automatic Dependent Surveillance‐Broadcast (ADS‐B) signal acquisition. The in‐orbit performance of the platform subsystems is also delivered in this paper. Thus, the successful design and development of SSS‐1 are explained and validated. Despite encountering challenges such as a single event upset (SEU) and attitude determination and control subsystem (ADCS) fault, SSS‐1's overall performance remained robust, and the fault's influence was greatly reduced with the manual control. This study not only highlights the technological advancements achieved by the SSS‐1 project but also provides valuable insights for future educational small satellite missions. [ABSTRACT FROM AUTHOR] |
| Copyright of International Journal of Aerospace Engineering is the property of Wiley-Blackwell 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 |
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| Header | DbId: egs DbLabel: Engineering Source An: 185963545 AccessLevel: 6 PubType: Academic Journal PubTypeId: academicJournal PreciseRelevancyScore: 0 |
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| Items | – Name: Title Label: Title Group: Ti Data: Exploring In‐Orbit Operations: Assessing Performance and Fault Management of the Student Small Satellite‐1 (SSS‐1). – Name: Author Label: Authors Group: Au Data: <searchLink fieldCode="AR" term="%22Liu%2C+Bohan%22">Liu, Bohan</searchLink><relatesTo>1,2</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Li%2C+Jia%22">Li, Jia</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Niu%2C+Xiaojie%22">Niu, Xiaojie</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Liu%2C+Yu%22">Liu, Yu</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Huang%2C+Hai%22">Huang, Hai</searchLink><relatesTo>1</relatesTo> (AUTHOR)<i> hhuang@buaa.edu.cn</i><br /><searchLink fieldCode="AR" term="%22Sun%2C+Liang%22">Sun, Liang</searchLink><relatesTo>1</relatesTo> (AUTHOR)<br /><searchLink fieldCode="AR" term="%22Habib%2C+Mohammad+Rezwan%22">Habib, Mohammad Rezwan</searchLink> (AUTHOR)<i> mohabib@wiley.com</i> – Name: TitleSource Label: Source Group: Src Data: <searchLink fieldCode="JN" term="%22International+Journal+of+Aerospace+Engineering%22">International Journal of Aerospace Engineering</searchLink>. 6/16/2025, Vol. 2025, p1-18. 18p. – Name: Subject Label: Subjects Group: Su Data: <searchLink fieldCode="DE" term="%22Microspacecraft%22">Microspacecraft</searchLink><br /><searchLink fieldCode="DE" term="%22Space+exploration%22">Space exploration</searchLink><br /><searchLink fieldCode="DE" term="%22Astronautics%22">Astronautics</searchLink><br /><searchLink fieldCode="DE" term="%22Propulsion+systems%22">Propulsion systems</searchLink><br /><searchLink fieldCode="DE" term="%22Technological+innovations%22">Technological innovations</searchLink> – Name: Abstract Label: Abstract Group: Ab Data: Small satellites represent a pivotal advancement in space technology, offering versatile platforms for conducting educational missions with reduced costs. Initiated by the Asia‐Pacific Space Cooperation Organization (APSCO), the Student Small Satellite‐1 (SSS‐1) mission exemplifies this paradigm. SSS‐1 is designed to validate the deployment of the coilable mast and conduct diverse space experiments in orbit. This paper provides a detailed exploration of the SSS‐1 space experiments and the fault handling procedures. Firstly, the overview of SSS‐1 is presented in this paper. Next, it details the results of various space experiments, including space imaging, remote sensing, electrical propulsion system tests, and Automatic Dependent Surveillance‐Broadcast (ADS‐B) signal acquisition. The in‐orbit performance of the platform subsystems is also delivered in this paper. Thus, the successful design and development of SSS‐1 are explained and validated. Despite encountering challenges such as a single event upset (SEU) and attitude determination and control subsystem (ADCS) fault, SSS‐1's overall performance remained robust, and the fault's influence was greatly reduced with the manual control. This study not only highlights the technological advancements achieved by the SSS‐1 project but also provides valuable insights for future educational small satellite missions. [ABSTRACT FROM AUTHOR] – Name: AbstractSuppliedCopyright Label: Group: Ab Data: <i>Copyright of International Journal of Aerospace Engineering is the property of Wiley-Blackwell 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: 10.1155/ijae/5971637 Languages: – Code: eng Text: English PhysicalDescription: Pagination: PageCount: 18 StartPage: 1 Subjects: – SubjectFull: Microspacecraft Type: general – SubjectFull: Space exploration Type: general – SubjectFull: Astronautics Type: general – SubjectFull: Propulsion systems Type: general – SubjectFull: Technological innovations Type: general Titles: – TitleFull: Exploring In‐Orbit Operations: Assessing Performance and Fault Management of the Student Small Satellite‐1 (SSS‐1). Type: main BibRelationships: HasContributorRelationships: – PersonEntity: Name: NameFull: Liu, Bohan – PersonEntity: Name: NameFull: Li, Jia – PersonEntity: Name: NameFull: Niu, Xiaojie – PersonEntity: Name: NameFull: Liu, Yu – PersonEntity: Name: NameFull: Huang, Hai – PersonEntity: Name: NameFull: Sun, Liang – PersonEntity: Name: NameFull: Habib, Mohammad Rezwan IsPartOfRelationships: – BibEntity: Dates: – D: 16 M: 06 Text: 6/16/2025 Type: published Y: 2025 Identifiers: – Type: issn-print Value: 16875966 Numbering: – Type: volume Value: 2025 Titles: – TitleFull: International Journal of Aerospace Engineering Type: main |
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