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  5. Development and Validation of the Operations Procedures and Manual for a 2U CubeSat, EIRSAT-1, with Three Novel Payloads
 
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Development and Validation of the Operations Procedures and Manual for a 2U CubeSat, EIRSAT-1, with Three Novel Payloads

Author(s)
Dunwoody, Rachel  
Doyle, Maeve  
Murphy, David  
Finneran, Gabriel  
O'Callaghan, Derek  
Reilly, Jack  
Thompson, Joseph W.  
Walsh, Sarah  
Erkal, Jessica  
Fontanesi, Gianluca  
Kyle, Jack  
Mangan, Joseph  
Marshall, Fergal  
Salmon, Lana  
de Faoite, Daithí  
Hanlon, Lorraine  
McKeown, David  
O'Connor, William  
Wall, Ronan  
McBreen, Sheila  
Uri
http://hdl.handle.net/10197/12232
Date Issued
2021-05-05
Date Available
2021-06-17T09:15:02Z
Abstract
The CubeSat standard, relatively short launch timescale, and orders of magnitude difference in cost in comparison to large scale missions, has allowed universities and smaller institutions to develop space missions. The Educational Irish Research Satellite (EIRSAT-1) is a 2U CubeSat being developed in University College Dublin (UCD) as part of the second round of the European Space Agency (ESA) Education Office’s Fly Your Satellite! (FYS) Programme. EIRSAT-1 is a student-led project to build, test, launch and operate Ireland’s first satellite. CubeSats typically use commercial off-the-shelf (COTS) components to facilitate new teams in developing a satellite on a rapid timescale. While some of the EIRSAT-1 subsystems are COTS procured from AAC Clyde Space, EIRSAT-1 has three novel experiments on-board which have been developed in UCD. The spacecraft’s Antenna Deployment Module has also been designed and built in-house. The on-board computer (OBC), procured from AAC Clyde Space, has been adapted to interface with these novel hardware components, accompanied by in-house developed software and firmware. All of these innovative subsystems complicate the CubeSat functionality making it essential to document and rigorously test the operations procedures for EIRSAT-1. In preparation for launch with these novel spacecraft subsystems, the EIRSAT-1 Operations Manual is being developed and incrementally verified. The Operations Manual contains the procedures to command and control the satellite, account for nominal and non-nominal scenarios and guide the operator in determining the cause of any anomalies observed during the mission and facilitate recovery. A series of operations development tests (ODTs) have been designed and conducted for a robust verification process. Each procedure is written up by a member of the EIRSAT-1 Operations Team in the EIRSAT-1 Operations Manual format. During an ODT, an in-flight scenario is considered in which the procedure under test is required. The procedure is then followed by a team member who has not been involved in the procedure development process. The feedback from these tests and from the operators is used to improve the procedures and continually update the Operations Manual. This paper will present the approach to operations development used by the EIRSAT-1 team and discuss the lessons learned for CubeSat operations development, testing and pre-flight verification.
Sponsorship
Irish Research Council
Science Foundation Ireland
Other Sponsorship
European Space Agency
Type of Material
Conference Publication
Copyright (Published Version)
2021 University College Dublin
Subjects

CubeSat

Spacecraft operations...

Fly Your Satellite!

EIRSAT-1

Web versions
https://spaceops2021.org/
Language
English
Status of Item
Peer reviewed
Conference Details
The 16th International Conference on Space Operations, Cape Town, South Africa, 3-5 May 2021
This item is made available under a Creative Commons License
https://creativecommons.org/licenses/by/3.0/ie/
File(s)
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Thumbnail Image
Name

SpaceOps-20212x1349.pdf

Size

2.9 MB

Format

Adobe PDF

Checksum (MD5)

ac28126619326c6732c399aa4a508886

Owning collection
Physics Research Collection
Mapped collections
Computer Science Research Collection•
Electrical and Electronic Engineering Research Collection•
Mechanical & Materials Engineering Research Collection

Item descriptive metadata is released under a CC-0 (public domain) license: https://creativecommons.org/public-domain/cc0/.
All other content is subject to copyright.

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