Please use this identifier to cite or link to this item:
https://doi.org/10.1109/AERO55745.2023.10115887
| DC Field | Value | |
|---|---|---|
| dc.title | Agile Development of Small Satellite's Attitude Determination and Control System | |
| dc.contributor.author | Foo, KJ | |
| dc.contributor.author | Tissera, MSC | |
| dc.contributor.author | Tan, RD | |
| dc.contributor.author | Low, KS | |
| dc.date.accessioned | 2023-06-26T11:36:39Z | |
| dc.date.available | 2023-06-26T11:36:39Z | |
| dc.date.issued | 2023-01-01 | |
| dc.identifier.citation | Foo, KJ, Tissera, MSC, Tan, RD, Low, KS (2023-01-01). Agile Development of Small Satellite's Attitude Determination and Control System. 2023 IEEE Aerospace Conference 2023-March. ScholarBank@NUS Repository. https://doi.org/10.1109/AERO55745.2023.10115887 | |
| dc.identifier.isbn | 9781665490320 | |
| dc.identifier.issn | 1095-323X | |
| dc.identifier.uri | https://scholarbank.nus.edu.sg/handle/10635/242519 | |
| dc.description.abstract | With the advanced development and maturing of small satellite technologies, there is a high commercial demand for low-cost small satellites with fast delivery for a multitude of applications. This paper presents a hardware-in-the-loop system for testing the satellite's attitude determination and control system and the Agile framework from software engineering practices to guide resource-effective end-to-end development processes, while maintaining a comprehensive system validation. Experimental results for design verification of satellite's Attitude Determination and Control Systems (ADCS) using our ongoing concurrent multiple satellite programs are presented. | |
| dc.publisher | IEEE | |
| dc.source | Elements | |
| dc.type | Conference Paper | |
| dc.date.updated | 2023-06-07T01:11:52Z | |
| dc.contributor.department | ELECTRICAL AND COMPUTER ENGINEERING | |
| dc.description.doi | 10.1109/AERO55745.2023.10115887 | |
| dc.description.sourcetitle | 2023 IEEE Aerospace Conference | |
| dc.description.volume | 2023-March | |
| dc.published.state | Published | |
| Appears in Collections: | Staff Publications Elements | |
Show simple item record
Files in This Item:
| File | Description | Size | Format | Access Settings | Version | |
|---|---|---|---|---|---|---|
| 2296_KJFoo_Agile Development of Small Satellite's Attitude Determination and Control System_Published.pdf | Published version | 1.45 MB | Adobe PDF | CLOSED | None |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.