Valente, Deoclecio und Schäfer, Andreas und Hoppe, Robert und Dressel, Frank (2025) A Holistic Framework for Uncertainty Quantification and Resilient Aircraft System Design. In: DLRK 2025, Seiten 1-17. DLRK2025, 2025-09-23 - 2025-09-25, Augsburg, Germany.
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Kurzfassung
In modern aircraft system development, uncertainty plays a critical role in shaping performance, safety, and certification outcomes. These uncertainties emerge across all stages of design and operation—ranging from material properties and aerodynamic loads to structural dynamics and control behavior. Addressing this complexity requires a structured, interdisciplinary approach that integrates quantitative analysis with engineering expertise. We propose a holistic, feedback-driven Uncertainty Quantification Framework (UQF) for aerospace systems engineering. The UQF couples \emph{six computational stages} with \emph{two governance layers} (expert-review gates and provenance/archiving with feedback), closing the loop by feeding insights back into models and data. A key differentiator is continuous collaboration with domain experts at each gate. A central innovation is the integration of provenance models, based on W3C PROV-O and implemented through \emph{provtool}, an open-source toolkit. Provenance containers trace inputs, tools, transformations, and agents, supporting digital continuity and certification-grade traceability. We demonstrate the UQF on a permanent-magnet synchronous motor (PMSM) within an electromechanical actuator. In this case, the UQF revealed an interaction-dominated structure and, via direct quasi--Monte Carlo propagation, verified the “ready-to-lock” speed requirement with substantial margin: no violations in $M=2^{20}$ samples (95\% Wilson upper bound ${\le} 3.7\times10^{-6}$) and a reliability-calibrated frontier near $430~\mathrm{rad/s}$ for a $10^{-3}$ risk target. All artifacts were captured as W3C PROV/SHACL bundles by \emph{provtool}, demonstrating auditability and reuse. While applied here to a single actuator subsystem, the framework is method- and use-case-agnostic and is scalable across aircraft domains. Ultimately, the UQF establishes a reproducible, modular, and certifiable methodology for design under uncertainty by embedding human expertise within a structured UQ process and enabling transparent data traceability. The results presented here were produced as part of the DLR internal project AdViCe (\textit{Advanced Methods for Virtual Certification}).
| elib-URL des Eintrags: | https://elib.dlr.de/222658/ | ||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
| Titel: | A Holistic Framework for Uncertainty Quantification and Resilient Aircraft System Design | ||||||||||||||||||||
| Autoren: |
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| Datum: | September 2025 | ||||||||||||||||||||
| Erschienen in: | DLRK 2025 | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| Seitenbereich: | Seiten 1-17 | ||||||||||||||||||||
| Herausgeber: |
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| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | Uncertainty Quantification, Aerospace Systems, PROV-O; Traceability, Certification; Electromechanical | ||||||||||||||||||||
| Veranstaltungstitel: | DLRK2025 | ||||||||||||||||||||
| Veranstaltungsort: | Augsburg, Germany | ||||||||||||||||||||
| Veranstaltungsart: | nationale Konferenz | ||||||||||||||||||||
| Veranstaltungsbeginn: | 23 September 2025 | ||||||||||||||||||||
| Veranstaltungsende: | 25 September 2025 | ||||||||||||||||||||
| Veranstalter : | DGLR | ||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||
| HGF - Programmthema: | Effizientes Luftfahrzeug | ||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
| DLR - Forschungsgebiet: | L EV - Effizientes Luftfahrzeug | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Virtuelles Flugzeug und Validierung | ||||||||||||||||||||
| Standort: | Braunschweig | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Flugsystemtechnik Institut für Softwaremethoden zur Produkt-Virtualisierung Institut für Flugsystemtechnik > Sichere Systeme und System Engineering | ||||||||||||||||||||
| Hinterlegt von: | Valente, Deoclecio | ||||||||||||||||||||
| Hinterlegt am: | 11 Feb 2026 09:22 | ||||||||||||||||||||
| Letzte Änderung: | 11 Feb 2026 09:22 |
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