98 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 98 total) Exploiting AI capabilities to facilitate and assist the evaluation process of ideas submitted in the OSIP platform – FEPOSI (Facilitating the Evaluation Process of Open Space Ideas) The general goal of this project is to operationalize and deepen the findings and conclusions of the initial project “Exploring AI capabilities to support the evaluation process of ideas submitted in the OSIP platform.” which demonstrated that AI techniques and software (COGITO Discover) could be used positively to enhance and ease the evaluation of ideas, by providing some new indicators such as idea novelty (scoring 0-100) based on the notion of similarity between ideas and innovation projects. Spain Discovery 21-D-O-TEC-02 EXPERT SYSTEM IBERIA SLU 2021 - 2022 Exploiting AI capabilities to facilitate and assist the evaluation process of ideas submitted in the OSIP platform – FEPOSI (Facilitating the Evaluation Process of Open Space Ideas) Augmented Reality for concurrent engineering activities During a multidisciplinary concurrent design activity, design data are shared via models edited by experts. Navigating and working on models - e.g. Plots, excel tables, Model Based Systems Engineering (MBSE) environments - describing very complex systems is a time consuming activity, prone to generate human errors. Augmented Reality (AR) technology shall be exploited in support of multidisciplinary design and review activities, reducing inconsistencies and enhancing intuitiveness. A number of solutions are available in non-space domain. Portugal TDE T708-607SY LUSOSPACE - PROJ DE ENGENHARIA 2019 - 2022 Augmented Reality for concurrent engineering activities Application of MBSE to reverse-engineer OPS-SAT and improve OPS-SAT2 The OPS-SAT MBSE activity had the 3 main objectives: France Discovery 20-D-S-OPS-01-a Samares Engineering 2021 - 2022 Application of MBSE to reverse-engineer OPS-SAT and improve OPS-SAT2 A Simulator for Marine Litter Observation from Space “Remote Sensing for Marine Litter - RESMALI” has identified the ideal parameters to study marine litter (ML) from space, including spectral bands with affordable signal-to-noise ratio (SNR) at top-of-atmosphere (TOA) level, in a range of wavelengths from visible to SWIR. To continue this path towards a dedicated mission, performance assessment against simulated real-case scenarios of ML is key. We want to build a simulator to estimate ML signal at TOA from a set of scenarios representing the various applications already targeted by the community (e.g. France Discovery 20-D-T-TEC-01-k ARGANS LIMITED 2020 - 2022 A Simulator for Marine Litter Observation from Space End-to-End System Engineering Portal (ESEP) Space system engineering is a complex activity, spanning multiple phases and involving different stakeholders using a variety of engineering approaches and tools. ESA has been investing in Model-Based System Engineering (MBSE) research for many years, developing different MBSE frameworks and Domain Specific Tools (DSTs). Recently, a broader need has been recognized to focus the MBSE efforts on semantic interoperability and associated model integration. Germany Discovery 20-D-T-TEC-04-d Spacecube GmbH 2020 - 2022 End-to-End System Engineering Portal (ESEP) Early in the loop MBSE assessment of electronic availability for nano/micro-satellites (ELMASAT) The main objective of the ELMASAT study was to brint into Capella the means to calculate the availability of a satellite system and provide extra facilities for trade-off analysis. As an example of application, an assesment of SEE detection and mitigation strategies was performed with respect to availability objectives. France Discovery 20-D-T-TEC-04-g IRT Saint-Exupery 2020 - 2022 Early in the loop MBSE assessment of electronic availability for nano/micro-satellites (ELMASAT) Application of MBSE to reverse-engineer OPS-SAT and improve OPS-SAT2 The main objective of the project is the reverse engineering of the OPS-SAT system, creating a model of the existing system design. The model aims to be built in a way that it is most useful for OPS-SAT engineers to understand and discuss the existing design and use this as a basis for further development of the OPS-SAT system. Germany Discovery 20-D-S-OPS-01-b OHB System AG 2021 - 2022 Application of MBSE to reverse-engineer OPS-SAT and improve OPS-SAT2 Procedure viewer and authoring tool for ground AIV/AIT applications Based on the existing international space station (ISS) procedure viewer capabilities it is proposed to develop a procedure viewer tool and related recording and authoring capabilities for ground based AIV/AIT activities on spacecraft. This tool shall allow a user friendly and easy generation of procedures that are typically used during spacecraft assembly, integration and test. Finland GSTP GT1P-001MX VTT TECHNICAL RESEARCH CENTRE OF FINLAND LTD 2019 - 2022 Procedure viewer and authoring tool for ground AIV/AIT applications Artificial intelligence (AI) and natural language processing (NLP) to support space engineering activities Model based approaches have proved to be efficient in supporting engineering activities, models replacing traditional document-based approaches. Nevertheless even in most advanced deployments, a lot of engineering artifacts are textual either because the return on investment of introducing models is too low on this particular case or because the information is more efficiently expressed in natural language even if consistency and correctness issues appears. France Discovery 20-D-T-TEC-04-n Thales Alenia Space 2020 - 2022 Artificial intelligence (AI) and natural language processing (NLP) to support space engineering activities De-risk assessment: Model Based FDIR design Today, spacecraft FDIR (Fault Detection, Isolation and Recovery) design is a time-consuming and error prone paper-based workflow, which does not help mastering the growing complexity of the space systems, and which mostly prevents early validation and verification of the design. Adequacy of the FDIR design is often assessed very late in the process (integration and test phase), sometimes even after the launch of the spacecraft (FDIR parameter tuning). 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