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The Low-Cost Attitude Determination and Control System ASTER: Design, Testing and Lessons Learned
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.
Luleå University of Technology, Department of Computer Science, Electrical and Space Engineering, Space Technology.ORCID iD: 0000-0003-3701-7925
2022 (English)In: IAC 2022 Congress Proceedings, 73rd International Astronautical Congress (IAC), International Astronautical Federation, IAF , 2022, article id 73838Conference paper, Published paper (Refereed)
Abstract [en]

The Attitude Determination and Control System (ADCS) of a spacecraft is often one of the most intricate subsystems, requiring significant resources to develop and integrate. An openly available ADCS platform for sounding rockets can make microgravity experiments more accessible, as development time and cost could be reduced. Project ASTER developed and tested such a solution. The main objective was to develop a low-cost and easy to manufacture system that enables future student teams and scientific missions with limited budget access to an experiment platform with a high-performance ADCS. The design utilises three reaction wheels, controlled by a closed-loop system, to stabilise a Free-Falling Unit ejected from a sounding rocket within seconds. The platform would be able to perform slewing manoeuvres and accommodate future experiments in an easily adaptable payload bay. The design and testing results are being published on an open-source basis allowing further improvement, optimisation, and customisation. ASTER was developed as part of the 13th cycle of the German-Swedish student programme REXUS/BEXUS and is scheduled to fly on REXUS-30 in March 2023. Due to the challenges faced by the project in the last phase of its development, the designed ADCS system will probably not be able to fly as a fully active payload on the REXUS rocket. The module will be assembled during the launch campaign in a reduced configuration and the flight will serve to verify the working systems such as the retention system designed by the team for large Free-Falling Units, as well as the mechanical low-cost design solution of the high-performance reaction wheels. Although the final technical issues encountered by the team during the experiment reviews could not be resolved completely as of now, the verification of the experiment subsystems in flight will be used to validate this initial design and enable further improvements. The project has pushed a team of students to design a very complex experiment and has helped them gain experience in dealing with common issues and failures faced in space projects. The paper will present the lessons learned from the overall project implementation and execution to help future student teams as well as the status of the additional flight opportunity.

Place, publisher, year, edition, pages
International Astronautical Federation, IAF , 2022. article id 73838
Series
Proceedings of the International Astronautical Congress, IAC, ISSN 0074-1795
Keywords [en]
Attitude Control, Lessons Learned, REXUS/BEXUS, Sounding Rocket, Student Experiment, Technology Demonstrator
National Category
Aerospace Engineering
Research subject
Atmospheric Science
Identifiers
URN: urn:nbn:se:ltu:diva-100696Scopus ID: 2-s2.0-85167599265OAI: oai:DiVA.org:ltu-100696DiVA, id: diva2:1790397
Conference
73rd International Astronautical Congress, IAC 2022, Paris, France, September 18-22, 2022
Available from: 2023-08-22 Created: 2023-08-22 Last updated: 2023-08-23Bibliographically approved

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Kuhn, Thomas

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