Please use this identifier to cite or link to this item:
https://doi.org/10.1109/AERO55745.2023.10115887
| Title: | Agile Development of Small Satellite's Attitude Determination and Control System | Authors: | Foo, KJ Tissera, MSC Tan, RD Low, KS |
Issue Date: | 1-Jan-2023 | Publisher: | IEEE | 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 | 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. | Source Title: | 2023 IEEE Aerospace Conference | URI: | https://scholarbank.nus.edu.sg/handle/10635/242519 | ISBN: | 9781665490320 | ISSN: | 1095-323X | DOI: | 10.1109/AERO55745.2023.10115887 |
| Appears in Collections: | Staff Publications Elements |
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| 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 |
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