Tuning of NASA Standard Breakup Model for Fragmentation Events Modelling Article Swipe
Nicola Cimmino
,
Giorgio Isoletta
,
Roberto Opromolla
,
Giancarmine Fasano
,
Aniello Basile
,
António Romano
,
Moreno Peroni
,
Alessandro Panico
,
Andrea Leonardo Cecchini
·
YOU?
·
· 2021
· Open Access
·
· DOI: https://doi.org/10.3390/aerospace8070185
YOU?
·
· 2021
· Open Access
·
· DOI: https://doi.org/10.3390/aerospace8070185
The continuous growth of space debris motivates the development and the improvement of tools that support the monitoring of a more and more congested space environment. Satellite breakup models play a key role to predict and analyze orbital debris evolution, and the NASA Standard Breakup Model represents a widely used reference, with current activities relevant to its evolution and improvements especially towards fragmentation of small mass spacecraft. From an operational perspective, an important point for fragmentation modelling concerns the tuning of the breakup model to achieve consistency with orbital data of observed fragments. In this framework, this paper proposes an iterative approach to estimate the model inputs, and in particular, the parents’ masses involved in a collision event. The iterative logic exploits the knowledge of Two Line Elements (TLE) of the fragments at some time after the event to adjust the input parameters of the breakup model with the objective of obtaining the same number of real fragments within a certain tolerance. Atmospheric re-entry is accounted for. As a result, the breakup model outputs a set of fragments whose statistical distribution, in terms of number and size, is consistent with the catalogued ones. The iterative approach is demonstrated for two different scenarios (i.e., catastrophic collision and non-catastrophic collision) using numerical simulations. Then, it is also applied to a real collision event.
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Metadata
- Type
- article
- Language
- en
- Landing Page
- https://doi.org/10.3390/aerospace8070185
- https://www.mdpi.com/2226-4310/8/7/185/pdf
- OA Status
- gold
- Cited By
- 13
- References
- 36
- Related Works
- 10
- OpenAlex ID
- https://openalex.org/W3179953612
All OpenAlex metadata
Raw OpenAlex JSON
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https://openalex.org/W3179953612Canonical identifier for this work in OpenAlex
- DOI
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https://doi.org/10.3390/aerospace8070185Digital Object Identifier
- Title
-
Tuning of NASA Standard Breakup Model for Fragmentation Events ModellingWork title
- Type
-
articleOpenAlex work type
- Language
-
enPrimary language
- Publication year
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2021Year of publication
- Publication date
-
2021-07-12Full publication date if available
- Authors
-
Nicola Cimmino, Giorgio Isoletta, Roberto Opromolla, Giancarmine Fasano, Aniello Basile, António Romano, Moreno Peroni, Alessandro Panico, Andrea Leonardo CecchiniList of authors in order
- Landing page
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https://doi.org/10.3390/aerospace8070185Publisher landing page
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https://www.mdpi.com/2226-4310/8/7/185/pdfDirect link to full text PDF
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YesWhether a free full text is available
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goldOpen access status per OpenAlex
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https://www.mdpi.com/2226-4310/8/7/185/pdfDirect OA link when available
- Concepts
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Breakup, Space debris, Collision, Computer science, Spacecraft, Fragmentation (computing), Aerospace engineering, Simulation, Physics, Mechanics, Engineering, Computer security, Operating systemTop concepts (fields/topics) attached by OpenAlex
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13Total citation count in OpenAlex
- Citations by year (recent)
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2025: 2, 2024: 3, 2023: 5, 2022: 3Per-year citation counts (last 5 years)
- References (count)
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36Number of works referenced by this work
- Related works (count)
-
10Other works algorithmically related by OpenAlex
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