Abstract
As Model-Based Systems Engineering (MBSE) continues to mature and becomes part of space engineering practice, the concept of a Reference Model becomes increasingly important. The CubeSat Reference Model (CRM) is an example of a reference model that is being developed by the INCOSE Space Systems Working Group (SSWG). The intent of the model is to facilitate the design, verification, and validation of CubeSat design. The CRM is being developed with sufficient flexibility to support customization for specific CubeSat missions by mission-specific CubeSat teams. This paper presents the key elements of the CRM developed using MBSE practices. It presents different views of the model along with a validation and verification approach. Further research is needed into how best to augment with other models to facilitate CubeSat test and evaluation.
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Acknowledgments
The authors acknowledge the contributions of SSWG team members Philip Cahill, Myron Hecht, and Brad Ayres in developing the Validation and Verification approaches expressed in this paper.
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Kaslow, D., Madni, A.M. (2018). Validation and Verification of MBSE-Compliant CubeSat Reference Model. In: Madni, A., Boehm, B., Ghanem, R., Erwin, D., Wheaton, M. (eds) Disciplinary Convergence in Systems Engineering Research. Springer, Cham. https://doi.org/10.1007/978-3-319-62217-0_27
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DOI: https://doi.org/10.1007/978-3-319-62217-0_27
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