| 1. |
- Alfredsson, Hampus, et al.
(author)
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Infrastructure modeling for large-scale introduction of electric aviation
- 2022
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In: 35th International Electric Vehicle Symposium and Exhibition (EVS35).
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Conference paper (peer-reviewed)abstract
- This paper presents the results of the MODELflyg research project funded by the Swedish Transport Administration to gain more knowledge about ground charging infrastructure demand for the electrification of air traffic. An integrated simulation model was developed including flight traffic data processing, modelling of battery electric aircraft performance, and charging simulations. Several different options are available to select specific air traffic flows of interest, including scheduling algorithms for electric aviation adapted timetables. Furthermore, a smart-charging algorithm was developed to lower peak power demand at each airport from simultaneous charging of multiple electric aircraft.
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| 2. |
- Alfredsson, Hampus, et al.
(author)
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Infrastrukturmodellering för storskalig introduktion av elflyg och flygtrafikledning (MODELflyg)
- 2022
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Reports (other academic/artistic)abstract
- En generisk, flexibel simuleringsmodell utvecklas med syftet att kunna bidra till förståelse samt ge möjligheter att enkelt testa vad elektrifiering (batterielektriskt) av önskade flygtrafikflöden kan förväntas innebära i form av krav på laddinfrastruktur vid flygplatserna. Modellen utvecklas i programspråket Python och innehåller ett flertal olika tillvägagångsätt för att testa elektrifiering såväl baserat på inläsning av historiska flygtrafikdata, som skapande av nya, icke-existerande flygtrafikscheman för elflyg. Eftersom det i dagsläget inte finns några elflygplan i kommersiell linjetrafik, och således inte heller någon data eller statistik gällande dess prestanda eller egenskaper, så utvecklas en modell även för detta, vilken tillåter simulering av önskade flygförbindelser, och resulterar i erhållande av energiförbrukning och flygtid på dessa. Projektet utgår ifrån en elflygplansmodell som är parametersatt i enlighet med certifieringsnivå CS/FAR-23 (19 säten och maxvikt 8618 kg). Logiken i modellen är att följa den fullständiga rörelsekedjan för varje flygplansindivid under en given tidsperiod (typiskt ett dygn), där behovet av laddning för respektive flygplan på respektive flygplats i kedjan ges av vilken energinivå batteriet höll vid påbörjad flygning, hur mycket energi som förbrukades under flygningen, när flygplanet anländer till destination, samt när det behöver påbörja nästa flygning. Även in- och uttaxning på flygplatserna påverkar hur mycket tid som finns tillgänglig för laddning. En inbyggd laddningskurva begränsar hur snabbt det är praktiskt lämpligt för batteriet att laddas. Laddningskurvan definieras genom ett förhållande mellan C-rate (Charging-rate) och SoC (State-of-Charge). Dessutom kan laddare i sig begränsas till en viss maxeffekt och styr således hur snabbt energi kan levereras till flygplanets batterier. För att möjliggöra tillräcklig räckvidd förväntas elflygplanen ha relativt stora batterier som dessutom sannolikt ska laddas upp inom korta tidsintervall på flygplatserna (turnaround-tider). Därmed kan behovet av installerad effektkapacitet förväntas öka drastiskt på flygplatserna om flera elflygplan behöver ladda samtidigt. Projektet lägger därför lite extra vikt vid att utveckla smarta algoritmer för styrning av effektuttag över tid med ambitionen att lastbalansera och sänka effekttoppar vid simultan laddning. Till sist diskuterar projektet vilka implikationer elflyg kan medföra ur perspektivet flygtrafikledning, befintliga och framtida luftrumsstrukturer. Ett flertal fallstudier genomförs för att exemplifiera modelleringsprocessen och de resultat som användaren slutligen får. Projektet syftar inte till att skapa något färdigt kommersiellt verktyg, utan snarare en första version, samt lägga grunden för vidareutveckling av ett analysverktyg som är till nytta för flygplatser och andra aktörer inom flygbranschen nu, och i framtida forskning- och utvecklingssamarbeten.
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| 3. |
- Amadori, Kristian, et al.
(author)
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Multidisciplinary Optimization of Wing Structure Using Parametric Models
- 2013
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Conference paper (other academic/artistic)abstract
- Aircraft design is an inherently multidisciplinary activity that requires integrating different models and tools to reach a well-balanced and optimized product. At Linköping University a design framework is being developed to support the initial design space exploration and the conceptual design phase. Main characteristics of the framework are its flexible database in XML format, together with close integration of automated CAD and other tools, which allows the developed geometry to be directly used in the subsequent preliminary design phase. In particular, the aim of the proposed work is to test the framework by designing, optimizing and studying a transport aircraft wing with respect to aerodynamic, geometry, structural and accessability constraints. The project will provide an initial assessment of the capability of the framework, both in terms of processing speed and accuracy of the results.
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| 4. |
- Axin, Mikael, 1984-, et al.
(author)
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Next Generation Simulation Software using Transmission Line Elements
- 2010
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In: Fluid Power and Motion Control. - : Centre for Power Transmission and Motion Control. - 9781861971814 ; , s. 265-276
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Conference paper (peer-reviewed)abstract
- A suitable method for simulating large complex dynamic systems is represented by distributed modelling using transmission line elements. The method is applicable to all physical systems, such as mechanical, electrical and pneumatics, but is particularly well suited to simulate systems where wave propagation is an important issue, for instance hydraulic systems. By using this method, components can be numerically isolated from each other, which provide highly robust numerical properties. It also enables the use of multi-core architecture since a system model can be composed by distributed simulations of subsystems on different processor cores.Technologies based on transmission lines has successfully been implemented in the HOPSAN simulation package, develop at Linköping University. Currently, the next generation of HOPSAN is developed using an object-oriented approach. The work is focused on compatibility, execution speed and real-time simulation in order to facilitate hardware-in-the-loop applications. This paper presents the work progress and some possible features in the new version of the HOPSAN simulation package.
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| 5. |
- Jouannet, Christopher, et al.
(author)
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Subscale flight testing used in conceptual design
- 2012
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In: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY. - : EMERALD GROUP PUBLISHING LIMITED. - 1748-8842 .- 0002-2667. ; 84:3, s. 192-199
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Journal article (peer-reviewed)abstract
- Purpose - The purpose of this paper is to present the latest subscale demonstrator aircraft developed at Linkoping University. It has been built as part of a study initiated by the Swedish Material Board (FMV) on a Generic Future Fighter aircraft. The paper will cover different aspects of the performed work: from paper study realised by SAAB to the first flight of the scaled demonstrator. The intention of the paper is to describe what has been realised and explain how the work is may be used to fit within aircraft conceptual design. Design/methodology/approach - The approach has been to address the challenges proposed by the customer of the demonstrator, how to design, manufacture and operate a scaled demonstrator of an aircraft study in conceptual design within five months. Similar research projects have been reviewed in order to perform the current work. Findings - The results obtained so far have led to new questions. In particular, the project indicated that more research is needed within the area of subscale flight testing for usage in aircraft conceptual design, since a scaled demonstrator is likely to answer some questions but will probably open up new ones. Research limitations/implications - The current research is just in its infancy and does not bring any final conclusion but does, however, offer several guidelines for future works. Since the aircraft study was an early phase concept study, not much data are available for validation or comparison. Therefore, the paper is not presenting new methods or general conclusions. Practical implications - Results from a conceptual aircraft study and a realisation of a scaled prototype are presented, which show that scaled flight testing may be used with some restriction in conceptual design. Originality/value - The value of this paper is to show that universities can be involved in prototype development and can work in close collaboration with industries to address issues and solutions within aircraft conceptual design.
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| 6. |
- Jouannet, Christopher, et al.
(author)
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SUSTAINABLE AVIATION FOR SWEDEN - TECHNOLOGY & CAPABILITY ASSESSMENT TARGETING 2045
- 2022
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In: 33rd CONGRESS OF THE INTERNATIONAL COUNCIL OF THE AERONAUTICAL SCIENCES. - 2958-4647.
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Conference paper (peer-reviewed)abstract
- The goal of this project is to analyse the possibilities offered by different technological solutions to achieve zero emission aviation, firstly in the Swedish/Nordic network context and secondly extend this to the European context. This project will investigate the potential and feasibility of new or upgraded aircraft types based on the different technologies mapped from both, various published roadmaps and national expertise from Swedish aerospace universities and companies. This involves developing aircraft conceptual designs studies and trade analysis with regards to different fuel types, propulsion technologies, structure, operations, network and fleet management, and all relevant technologies. The project will, on a common technology basis, analyse a range of zero carbon fuels and associated technologies through operational studies and optimization to accelerate the introduction of fossil free aircraft technology and choosing optimal paths for making aviation sustainable.
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| 7. |
- Knöös Franzén, Ludvig, 1990-, et al.
(author)
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A Breakdown of System of Systems Needs Using Architecture Frameworks, Ontologies and Description Logic Reasoning
- 2021
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In: Aerospace. - : MDPI. - 2226-4310. ; 8:4
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Journal article (peer-reviewed)abstract
- Aerospace systems are connected with the operational environment and other systems in general. The focus in aerospace product development is consequently shifting from a singular system perspective to a System-of-Systems (SoS) perspective. This increasing complexity gives rise to new levels of uncertainty that must be understood and managed to produce aerospace solutions for an ever-changing future. This paper presents an approach to using architecture frameworks, and ontologies with description logic reasoning capabilities, to break down SoS needs into required capabilities and functions. The intention of this approach is to provide a consistent way of obtaining the functions to be realized in order to meet the overarching capabilities and needs of an SoS. The breakdown with an architecture framework results in an initial design space representation of functions to be performed. The captured knowledge is then represented in an ontology with description logic reasoning capabilities, which provides a more flexible way to expand and process the initial design space representation obtained from the architecture framework. The proposed approach is ultimately tested in a search and rescue case study, partly based on the operations of the Swedish Maritime Administration. The results show that it is possible to break down SoS needs in a consistent way and that ontology with description logic reasoning can be used to process the captured knowledge to both expand and reduce an available design space representation.
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| 8. |
- Knöös Franzén, Ludvig, 1990-, et al.
(author)
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A System of Systems Approach for Search and Rescue Missions
- 2020
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Conference paper (peer-reviewed)abstract
- System-of-Systems Engineering (SoSE) has become a constantly growing field within product development for complex systems. Systems are becoming more and more connected with other systems and the operational environment in general. This takes the development process to new levels of complexity where high degrees of uncertainties are expected due to ever occurring changes in the operational environment, and other external factors such as politics, economy, and technology. This creates a need of being able to understand the influence of changes early in the development process and to facilitate the systems? perseverance. The focus of the development shifts from fulfilling specific requirements, to being able to meet needs and deliver capabilities over time. Additionally, modeling and simulation for complex systems and System-of-Systems (SoS) becomes a valued alternative to the economically prohibited and almost impossible prototype testing. In consideration of this problem, the presented work introduces a method for both modeling and simulation of a SoS. The method uses ontology with description logic reasoning to derive and narrow down a SoS design space which is further analyzed using Agent Based Simulation (ABS). A Search and Rescue (SAR) scenario is used as a case study to test the method. Measures of Effectiveness (MoE), based on the time it takes to find a rescue subject and the cost of doing so, are used to evaluate the SoS performances. The presented method is envisioned to be used early in the development of complex systems and SoS to increase the overall understanding of them.
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| 9. |
- Knöös Franzén, Ludvig, 1990-
(author)
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A System of Systems View in Early Product Development : An Ontology-Based Approach
- 2023
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Doctoral thesis (other academic/artistic)abstract
- The concept of system-of-systems is becoming increasingly common and relevant in many engineering applications. Today’s highly interconnected world entails that more and more systems have dependencies on other systems. This increasing number of interdependencies results in new levels of complexity that must be managed in the early development of new products. Different viewpoints must also be handled to understand the many layers of a system-of-systems and its surrounding context. An ever-changing future results in uncertainty about the operational environment but also other aspects, such as available technologies, which complicates the matter even further. Traditional approaches for early product development can be used to some extent, but the complexity, scale and sheer number of interconnections in system-of-systems require a holistic perspective to obtain an early understanding of the problem, design spaces, and multiple aspects involved. This dissertation aims to present a method that has been developed to address the demand for a more holistic system-of-systems view in early product development. Overall, the method consists of four parts that together show how design spaces for system-of-systems can be generated and later processed to find suitable solutions. Search and rescue operations have been used as examples of system-of-systems throughout this work and in the development of the presented method. The first two parts of the method are based on architecture frameworks and ontologies with description logic reasoning capabilities. An architecture framework is here used to break down system-of-system needs into functions to be fulfilled by constituent systems. Ontologies are thereafter used to represent the outcome and the resulting system-of-system design spaces with involved entities and their relationships. Description logic reasoning can subsequently be used to process the available design spaces and suggest suitable system-of-system solutions. The last two parts of the method build upon a concept exploration and estimation approach, together with visual analytics. The approach illustrates how individual system concepts can be estimated from an ontology-represented design space, and how visual analytics can be used to explore different system-of-system viewpoints at an early stage. Based on the outcomes of the presented method, this dissertation contributes a holistic take on early product development from a system-of-systems perspective.
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| 10. |
- Knöös Franzén, Ludvig, 1990-
(author)
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An Ontological and Reasoning Approach to System of Systems
- 2021
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Licentiate thesis (other academic/artistic)abstract
- System-of-Systems (SoS) are all around us and are becoming more common in today’s highly interconnected world. Systems are connected with other systems and have strong dependencies with their operational environments. This leads to an increased level of complexity and risk during product development. A holistic view, and an SoS perspective, is consequently needed in order to develop an early understanding of the available design spaces for new system solutions. This thesis suggests a method that has been developed for this purpose, and to meet the demand for a more holistic product development. Overall, the method consists of two correlated approaches that show how a design space for SoSs can be generated and later processed with, for example, design space reductions. Search and Rescue (SAR) operations have been used as examples of typical SoSs throughout this work and in the development of the presented method. An architecture framework has been used to introduce a standardized and consistent way of understanding the relationships that exist between needs, capabilities and functions. This approach can consequently be used to generate a design space of functions to be performed to meet the overarching needs of an SoS. The second approach has been based on ontology and description logic reasoning. Ontology has here been used to represent an SoS design space with, for example, available SAR assets and their relationships with the operational environment. An SoS representation in an ontology model introduces additional expressiveness and the design space processing capabilities needed for a holistic design process and product development. Based on these results, this thesis and its suggested method and approaches contribute to holistic product development from an SoS perspective.
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