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Dissertations / Theses on the topic 'Avionic systems'

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Published: 4 June 2021

Last updated: 25 May 2024

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1

Jones, Andy. "Component-led integrative optimisation methodology for avionic thermal management." Thesis, Loughborough University, 2017. https://dspace.lboro.ac.uk/2134/24785.

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The modern military aircraft can be defined as a System of Systems (SoS); several distinct systems operating simultaneously across boundary interfaces. As the on-board subsystems have become more complex and diverse, the development process has become more isolated. When considering thermal management of distributed heat loads, the aircraft has become a collection of individually optimised components and subsystems, rather than the implementation of a single system to perform a given task. Avionic thermal management is quickly becoming a limiting factor of aircraft performance, reliability and

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2

Al, Sheikh Ahmad. "Resource allocation in hard real-time avionic systems : scheduling and routing problems." Phd thesis, INSA de Toulouse, 2011. http://tel.archives-ouvertes.fr/tel-00631443.

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Le domaine avionique a été transformé par l'apparition des architectures modulaires intégrées (IMA). Celles-ci définissent un support d'exécution et de communication standard et mutualisé afin de réduire la complexité de l'architecture physique. Cependant, du fait du partage des ressources, cette démarche introduit une plus grande complexité lors de la conception et de l'intégration des applications ce qui implique d'assister les concepteurs avec des outils dédiés. La présente thèse contribue à cet effort en se focalisant sur deux problèmes d'allocation de ressources : i) le problème de l'ordo

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3

Al, Sheikh Ahmad. "Resource allocation in hard real-time avionic systems : scheduling and routing problems." Electronic Thesis or Diss., Toulouse, INSA, 2011. http://www.theses.fr/2011ISAT0010.

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Le domaine avionique a été transformé par l'apparition des architectures modulaires intégrées (IMA). Celles-ci définissent un support d'exécution et de communication standard et mutualisé afin de réduire la complexité de l'architecture physique. Cependant, du fait du partage des ressources, cette démarche introduit une plus grande complexité lors de la conception et de l'intégration des applications ce qui implique d’assister les concepteurs avec des outils dédiés. La présente thèse contribue à cet effort en se focalisant sur deux problèmes d'allocation de ressources : i) le problème de l'ordo

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4

Harwood, Donald James. "Graphics system enhancement using post raster processors." Thesis, University of Bristol, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.361139.

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5

Wikman, Kasper. "Integration of Orbital Control in the Avionic Test-Bench Simulators for EagleEye : Evolution of the EagleEye functionality." Thesis, Luleå tekniska universitet, Institutionen för system- och rymdteknik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-76114.

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In the space industry a lot of efforts is put towards verification and validationof the different parts of the spacecraft. This is a costly process and cause initial friction when trying to introduce new technology within the field. One of the demanding systems to validate and test is the on-board software. To makethe process of evaluation and testing of new technologies easier, the EuropeanSpace Agency has put effort towards creating an end-to-end avionic test bench containing four different simulators. In this test bench a fictional mission called EagleEye was constructed. EagleEye is a repr

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6

Gatti, Marc. "Évolution des Architectures des Systèmes Avioniques Embarqués." Thesis, Paris 6, 2016. http://www.theses.fr/2016PA066725/document.

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De nos jours, les systèmes embarqués sont les éléments Cœurs des Systèmes avioniques. De plus en plus de fonctions sont intégrées et de ce fait leurs complexités croît. Afin que cette complexité puisse rester maîtrisable, l’architecture des systèmes avionique a également évolué de façon à minimiser les interactions entre les équipements. Cette évolution des Architectures a introduit, au niveau avionique, la notion de réseau largement répandue dans le monde dit « consumer ». Nos travaux de Recherche ont pour but d’accompagner cette évolution architecturale en minimisant l’impact des ruptures te

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7

ESPOSITO, STEFANO. "Mixed-Criticality Systems on Commercial-Off-the-Shelf Multi-Processor Systems-on-Chip." Doctoral thesis, Politecnico di Torino, 2018. http://hdl.handle.net/11583/2706773.

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Avionics and space industries are struggling with the adoption of technologies like multi-processor system-on-chips (MPSoCs) due to strict safety requirements. This thesis propose a new reference architecture for MPSoC-based mixed-criticality systems (MCS) - i.e., systems integrating applications with different level of criticality - which are a common use case for aforementioned industries. This thesis proposes a system architecture capable of granting partitioning - which is, for short, the property of fault containment. It is based on the detection of spatial and temporal interference

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8

Gatti, Marc. "Évolution des Architectures des Systèmes Avioniques Embarqués." Electronic Thesis or Diss., Paris 6, 2016. https://accesdistant.sorbonne-universite.fr/login?url=https://theses-intra.sorbonne-universite.fr/2016PA066725.pdf.

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De nos jours, les systèmes embarqués sont les éléments Cœurs des Systèmes avioniques. De plus en plus de fonctions sont intégrées et de ce fait leurs complexités croît. Afin que cette complexité puisse rester maîtrisable, l’architecture des systèmes avionique a également évolué de façon à minimiser les interactions entre les équipements. Cette évolution des Architectures a introduit, au niveau avionique, la notion de réseau largement répandue dans le monde dit « consumer ». Nos travaux de Recherche ont pour but d’accompagner cette évolution architecturale en minimisant l’impact des ruptures te

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9

Gustavsson, Henrik. "Utvärdering av simulatorer och emulatorer för inbyggda system." Thesis, Tekniska Högskolan, Högskolan i Jönköping, JTH, Data- och elektroteknik, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-17983.

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Uppdragsgivaren Saab Electronic Defence Systems i Jönköping erbjuder ett flertal produkter främst inom avioniksystem. För att kunna utvärdera och kontrollera produktens design i ett tidigt skede så kan en simulering av systemets beteende och att felsöka så tidigt som möjligt vara ett möjligt alternativ. En systemsimulering kan innebära att mjukvaruutveckling och felsökning kan påbörjas långt innan hårdvaruprototypen är tillgänglig, med samma storlek och komplexitet som systemet. Andra fördelar med simulering är att det går enklare att fastställa orsaken till systemkrasch, hitta de längsta exek

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10

Switzer, Earl, Michael Whelan, and Farncisco Lagunas. "AIR TRAFFIC CONTROL COMMUNICATIONS TEST FACILITY AND AVIONICS SYSTEM TEST (ACTFAST): GEARING UP FOR NEXT GENERATION AVIONICS SYSTEMS TESTING." International Foundation for Telemetering, 2000. http://hdl.handle.net/10150/608285.

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International Telemetering Conference Proceedings / October 23-26, 2000 / Town & Country Hotel and Conference Center, San Diego, California<br>Growth in civil aviation is overwhelming worldwide airspace and air traffic services. The International Civil Aviation Organization (ICAO), Federal Aviation Administration (FAA) and Department of Defense (DoD) are proposing or implementing numerous changes to address this growth. The changes are broadly contained in what the civil aviation community calls Communication, Navigation, and Surveillance/Air Traffic Management (CNS/ATM) and the DoD calls Glob

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11

Karlsson, Emil. "Optimisation-based scheduling of an avionic system." Licentiate thesis, Linköpings universitet, Optimeringslära, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-156695.

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Modern computer systems in aircraft are often based on an integrated modular avionic architecture. In this architecture, software applications share hardware resources on a common avionic platform. Many functions in an aircraft are controlled by software and a failure in such software can have severe consequences. In order to avoid malfunction, there are many aspects to consider. One aspect is to ensure that the activities in the system is done at the right time with the right resources. To analyse if this is possible or not is often called schedulability analysis. When multiple functions are

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12

Paquette, Jean J. R. Carleton University Dissertation Engineering Electrical. "The Next generation avionic system; a prediction." Ottawa, 1985.

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13

Druetta, Elisa. "Avionic retrofit of a Piper PA-32R-300: system analysis for glass cockpit avionic conversion." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2017.

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This thesis project concerns the design of the avionic retrofit for a Piper PA-32R-300 cockpit. The work was developed as a collaborative project performed at DigiSky and it led to the detailed design of a new Glass Cockpit. A complete design process was addressed starting with the exploration of some possible configurations, with all the feasibility analysis coming to the selection of a configuration, its optimization and the editing of the Service Bulletin.

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14

Sukardjo, Wishnu. "Methods of avionics systems maintenance procedures." Thesis, University of Central Lancashire, 1995. http://clok.uclan.ac.uk/21166/.

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Avionics System Maintenance Procedures are discussed in this thesis in the context of a BPhil project involving formal training in research methods and includes information obtained by investigating issues pertinent to aircraft avionics systems maintenance. Personnel matters, problem specification and identification, maintenance procedures, health and safety issues, and quality control issues are discussed in terms of their influence in effectively carrying out required maintenance. The work described in the thesis demonstrates that several research methods are applicable to, and effective for

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15

Tondreault, Jeremy P. (Jeremy Peter) 1973. "Improving the management of system development to produce more affordable military avionics systems." Thesis, Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/82698.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design & Management Program, 2003.<br>This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.<br>"February 2003."<br>Includes bibliographical references (p. 126-127).<br>by Jeremy P. Tondreault.<br>S.M.

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Gavrilets, Vladislav 1975. "Avionics systems development for small unmanned aircraft." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/50382.

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17

Dessiatnikoff, Anthony. "Analyse de vulnérabilités de systèmes avioniques embarqués : classification et expérimentation." Phd thesis, INSA de Toulouse, 2014. http://tel.archives-ouvertes.fr/tel-01032444.

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L'évolution actuelle des systèmes embarqués à bord des systèmes complexes (avions, satellites, navires, automobiles, etc.) les rend de plus en plus vulnérables à des attaques, en raison de : (1) la complexité croissante des applications ; (2) l'ouverture des systèmes vers des réseaux et systèmes qui ne sont pas totalement contrôlés ; (3) l'utilisation de composants sur étagère qui ne sont pas développés selon les méthodes exigées pour les systèmes embarqués critiques ; (4) le partage de ressources informatiques entre applica- tions, qui va de pair avec l'accroissement de puissance des processe

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18

Löfwenmark, Andreas. "Timing Predictability in Future Multi-Core Avionics Systems." Licentiate thesis, Linköpings universitet, Programvara och system, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-134427.

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With more functionality added to safety-critical avionics systems, new platforms are required to offer the computational capacity needed. Multi-core platforms offer a potential that is now being explored, but they pose significant challenges with respect to predictability due to shared resources (such as memory) being accessed from several cores in parallel. Multi-core processors also suffer from higher sensitivity to permanent and transient faults due to shrinking transistor sizes. This thesis addresses several of these challenges. First, we review major contributions that assess the impact o

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19

Black, James A. "HIGH SPEED AVIONICS DATA INSTRUMENTATION SYSTEM (HADIS)." International Foundation for Telemetering, 1992. http://hdl.handle.net/10150/608905.

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International Telemetering Conference Proceedings / October 26-29, 1992 / Town and Country Hotel and Convention Center, San Diego, California<br>SAIC, under contract with the Air Force Wright Laboratory, has developed and demonstrated a prototype High Speed Avionics Data Instrumentation System (HADIS). The HADIS system is designed to operate in both the laboratory and in an airborne environment. This paper briefly describes the features of the system including its ability to collect and record data at up to 13.25 MBytes per second, its ability to provide real-time processing of the data,

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20

Block, Max. "Pre-Runtime Scheduling of an Avionics System." Thesis, Uppsala universitet, Institutionen för informationsteknologi, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-300679.

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This master's thesis addresses a scheduling problem arising when designing avionics – the electronic systems used on aircraft. Currently, the problem is commonly solved using mixed integer programming (MIP). We prove the scheduling problem at-hand, which is similar to the well-studied cyclic job shop scheduling problem, is NP-hard. Furthermore, we propose an approach using constraint programming (CP) – a programming paradigm where entities called constraints define the relations between variables. Constraints do not specify a step or sequence of steps to execute, but rather the necessary prope

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21

Enkvist, Clas. "Integrerad modulär avionik med virtualisering." Thesis, Linköpings universitet, Institutionen för datavetenskap, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-98433.

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Det finns huvudsakligen tre olika sätt att konstruera ett partitionerat system på: Federerad arkitektur, Integrerad Modulär Avionik (IMA) med ARINC 653 eller IMA med virtualisering. I den här rapporten undersöks de olika arkitekturernas egenskaper och vilka möjligheter som finns för certifiering av dem. Efter den teoretiska undersökningen har Virtualisering, och framförallt Xen, valts ut för en testimplementation och tillförlitlighetstester. Testimplementationen består av fyra partitioner där varje partition har sin specifika uppgift att lösa. Den fjärde partitionen används för att undersöka h

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22

Vetter, David B. (David Brian). "Design of multi-passage cooling systems for avionics applications." Thesis, Massachusetts Institute of Technology, 1993. http://hdl.handle.net/1721.1/115475.

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23

Plew, Jason. "Development of a flight avionics system for an autonomous Micro Air Vehicle." [Gainesville, Fla.] : University of Florida, 2004. http://purl.fcla.edu/fcla/etd/UFE0008540.

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24

Erdinc, Emre. "Soft Afdx (avionics Full Duplex Switched Ethernet) End System Implementation With Standard Pc And Ethernet Card." Master's thesis, METU, 2010. http://etd.lib.metu.edu.tr/upload/12611929/index.pdf.

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ARINC 664/AFDX (Avionics Full Duplex Switched Ethernet) protocol is a leading onboard communication technology in civil aviation. As AFDX is a new technology, unit cost of the hardware devices are high and protocol is open to changes. This thesis discusses the design of an AFDX End System application for test environment with a software based solution with cheap COTS (Commercial offthe shelf) equipment, explains the implementation of the software and analysis the performance.

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25

Andersson, Henric. "Aircraft Systems Modeling : Model Based Systems Engineering in Avionics Design and Aircraft Simulation." Licentiate thesis, Linköping University, Linköping University, Machine Design, 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17573.

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<p>Aircraft developers like other development and manufacturing companies, are experiencing increasing complexity in their products and growing competition in the global market. One way to confront the challenges is to make the development process more efficient and to shorten time to market for new products/variants by using design and development methods based on models. Model Based Systems Engineering (MBSE) is introduced to, in a structured way, support engineers with aids and rules in order to engineer systems in a new way.</p><p>In this thesis, model based strategies for aircraft and avi

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Bilen, Celal Can, and John Alcalde. "Performance Evaluation of Embedded Microcomputers for Avionics Applications." Thesis, Jönköping University, JTH, Computer and Electrical Engineering, 2010. http://urn.kb.se/resolve?urn=urn:nbn:se:hj:diva-11955.

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<p>Embedded microcomputers are used in a wide range of applications nowadays. Avionics is one of these areas and requires extra attention regarding reliability and determinism. Thus, these issues should also be born in mind in addition to performance when evaluating embedded microcomputers.</p><p>This master thesis suggests a framework for performance evaluation of two members of the PowerPC microprocessor family, namely the MPC5554 from Freescale and PPC440EPx from AMCC, and analyzes the results within and between these processors. The framework can be generalized to be used in any microproce

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27

Omelchenko, Alexander 1968. "Avionics systems design for cooperative unmanned air and ground vehicles." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/17789.

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Thesis (S.M. and E.A.A.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.<br>"June 2004."<br>Includes bibliographical references (p. 95).<br>This thesis summarizes the results of the design of avionics systems intended for use onboard unmanned air and ground vehicles, that are parts of a multi-vehicle system whose primary mission objective is to provide up-close surveillance capability from a large stand-off distance. Different types of cooperative action between air and ground vehicles, that can help to enhance the overall system surveillance capability, ar

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28

Thenent, Nils Elias. "The representation of an advanced service delivered by a product service system : a qualitative model of avionics availability." Thesis, University of Bath, 2014. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.629659.

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The research presented in this thesis demonstrates the qualitative modelling of an advanced service delivered by a Product Service System (PSS) through the use of a socio-technical systems-based approach. The created model represents dependencies between functions and organisations, and can be used as basis for a quantitative cost model. Focus is on how one particular example of advanced services, namely availability is delivered in an industrial context. Following a review of multi-disciplinary literature and the outline of a suitable methodological approach, a detailed case study of the deli

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29

Kahn, Aaron David. "The design and development of a modular avionics system." Thesis, Georgia Institute of Technology, 2001. http://hdl.handle.net/1853/15712.

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Graziano, Timothy Michael. "Establishment of a Cyber-Physical Systems (CPS) Test Bed to Explore Traffic Collision Avoidance System (TCAS) Vulnerabilities to Cyber Attacks." Thesis, Virginia Tech, 2021. http://hdl.handle.net/10919/104624.

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Traffic Collision Avoidance Systems (TCAS) are safety-critical, unauthenticated, ranging systems required in commercial aircraft. Previous work has proposed TCAS vulnerabilities to attacks from malicious actors with low cost software defined radios (SDR) and inexpensive open-source software (GNU radio) where spoofing TCAS radio signals in now possible. This paper outlines a proposed threat model for several TCAS vulnerabilities from an adversarial perspective. Periodic and aperiodic attack models are explored as possible low latency solutions to spoof TCAS range estimation. A TCAS test bed is

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Nguyen, Anh-Minh Ngoc. "High-Quality Detection in Heavy-Traffic Avionic Communication System Using Interference Cancellation Techniques." Diss., Virginia Tech, 2005. http://hdl.handle.net/10919/29069.

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This dissertation focuses on quantifying the effects of multi-user co-channel interference for an avionic communication system operating in a heavy-traffic aeronautical mobile environment and proposes advanced interference cancellation techniques to mitigate the interference. The dissertation consists of two parts. The first part of the work investigates the use of a visualization method to quantify and characterize the multi-user co-channel interference (multiple access interference) effects impinging on an avionic communication system. The interference is caused by complex interactions of

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Dova, Vincent H. "Software-defined avionics and mission systems in future vertical lift aircraft." Thesis, Monterey, California: Naval Postgraduate School, 2015. http://hdl.handle.net/10945/45181.

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Approved for public release; distribution is unlimited<br>Integrated Modular Avionics, or IMA, has been a notable trend in aircraft avionics for the past two decades, promising significant size, weight, and power-consumption (SWAP) gains, radically increased sensors fusion, and streamlined support costs. Despite the demonstrated success of IMA systems in commercial airliners such as the Airbus A380 and the Boeing 787, military rotorcraft in the service of the United States Joint services have yet to benefit significantly from this technology. At long last, that may be about to change. The Futu

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Wölfl, Andreas [Verfasser], and Harald [Akademischer Betreuer] Kosch. "Data Management in Certified Avionics Systems / Andreas Wölfl ; Betreuer: Harald Kosch." Passau : Universität Passau, 2018. http://d-nb.info/1168473349/34.

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34

Rauch, William D. "TELEMETRY SYSTEMS OF THE FUTURE." International Foundation for Telemetering, 1989. http://hdl.handle.net/10150/614480.

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International Telemetering Conference Proceedings / October 30-November 02, 1989 / Town & Country Hotel & Convention Center, San Diego, California<br>The next 25 years will bring about a revolution in telemetry acquisition and processing. Airborne systems will become smaller and faster, providing additional monitoring and processing capabilities to test vehicles. In addition, ultra-high speed on-board data networks will provide communications between data collection and processing units. The telemetry platforms of tomorrow will be required to collect the entire contents of the data network, in

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Greer, Daniel S. "Avionics System development for a Rotary Wing Unmanned Aerial Vehicle." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1998. http://handle.dtic.mil/100.2/ADA350437.

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Thesis (M.S. in Aeronautical Engineering) Naval Postgraduate School, June 1998.<br>"June 1998." Thesis advisor(s): Russ W. Duren. Includes bibliographical references (p. 79). Also available online. Mode of access: World Wide Web.

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Doverfelt, Rickard. "An Evaluation of Ethernet as Data Transport System in Avionics." Thesis, KTH, Skolan för elektroteknik och datavetenskap (EECS), 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-284584.

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ÅF Digital Solutions AB are looking to replace their current legacy system for audio transmissions within aircrafts with a new system based on Ethernet. They also want the system to be as closely matching the current Audio Integration System as possible as well as preferably using commercial off the shelf components. The issue evaluated in this thesis is whether it is feasible to port the legacy protocol over to an Ethernet based solution with as few modifications as possible, what performance requirements are present on the Ethernet solution as well as what remaining capacity is available in

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Aman, Shah Shahani. "System level airborne avionics prognostics for maintenance, repair and overhaul." Thesis, Cranfield University, 2016. http://dspace.lib.cranfield.ac.uk/handle/1826/11844.

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The aim of this study is to propose an alternative approach in prognostics for airborne avionics system in order to enhance maintenance process and aircraft availability. The objectives are to analyse the dependency of avionic systems for fault propagation behaviour degradation, research and develop methods to predict the remaining useful life of avionics Line Replaceable Units (LRU), research and develop methods to evaluate and predict the degradation performances of avionic systems, and lastly to develop software simulation systems to evaluate methods developed. One of the many stakeholders

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Riebeling, Rolf-Rekke [Verfasser]. "Modellgetriebene, wissensbasierte Entwicklung von Avionik-Systemen / Rolf-Rekke Riebeling." München : Verlag Dr. Hut, 2018. http://d-nb.info/1164293451/34.

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Duym, Wade Douglas. "Effects of digital avionics systems on the survivability of modern tactical aircraft." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1995. http://handle.dtic.mil/100.2/ADA303313.

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Tal, Oded. "Software dependability demonstration for safety-critical military avionics systems by statistical testing." Thesis, Nottingham Trent University, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.266819.

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Wegener, John A., and Robert N. Zettwoch. "AN INSTRUMENTATION CONTROL SYSTEM THAT UTILIZES AN AVIONICS PILOT DISPLAY INTERFACE." International Foundation for Telemetering, 2004. http://hdl.handle.net/10150/604958.

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International Telemetering Conference Proceedings / October 18-21, 2004 / Town & Country Resort, San Diego, California<br>Flight Test instrumentation control units have traditionally been low-technology units with mechanical switches, readouts, and perhaps an RS232 interface. As the complexity of Flight Test Instrumentation systems and operational requirements increase, and as cockpit space becomes scarce, these control units are no longer sufficient. These control units need to provide capabilities commensurate with the complexity of the instrumentation systems they control. This paper d

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Mehmood, Qaiser. "A Maintainability Analysis of Dependability Evaluation of an Avionic System using AADL to PNML Transformation." Thesis, Blekinge Tekniska Högskola, Institutionen för programvaruteknik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:bth-12807.

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Context.In the context of Software Architecture, AADL (ArchitectureAnalysis and Design Language) is one of the latest standards (SAE StandardAS5506) used for analyzing and designing of architectures of software sys-tems. Dependability evaluation of an avionic system, modeled in AADL, isconducted using petri nets standard PNML (ISO standard ISO/IEC15909-2).A maintainability analysis of PNML dependability model is also con-ducted. Objectives. In this study we investigate maintainability analysis of PNMLdependability model of an avionic system designed in AADL. Structural,functional, fault-tolera

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Salley, Thomas, and Steven E. Thorssell. "AN ALTERNATIVE METHOD FOR ACQUIRING AVIONIC BUS DATA IN A CLASS I PCM TELEMETRY SYSTEM." International Foundation for Telemetering, 1992. http://hdl.handle.net/10150/613141.

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International Telemetering Conference Proceedings / October 26-29, 1992 / Town and Country Hotel and Convention Center, San Diego, California<br>IRIG 106-86 Chapter 8 describes the standard for acquisition of MIL-STD-1553 traffic flow. All incoming words (command, status, or data) are transmitted and fill words are used to maintain continuous data output. If all incoming words are not needed, or if other data such as sampled analog data from transducers are also to be transmitted, then a different approach is warranted. Selected data from the avionics bus can be placed into predefined PCM word

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Meredith, Andrew. "Use of wireless sensor networks to supplement arinc 429 on aircraft avionics systems." Thesis, California State University, Long Beach, 2014. http://pqdtopen.proquest.com/#viewpdf?dispub=1527397.

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Kovalenko, Yuliia. "Principles of organizing the architecture of perspective onboard digital computing systems in avionics." Thesis, National Aviation University, 2021. https://er.nau.edu.ua/handle/NAU/50995.

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1. Konakhovych H., Kozlyuk I., Kovalenko Y. (2020) Specificity of optimization of performance indicators of technical operation and updating of radio electronic systems of aircraft. System research and information technologies, no. 3, pp. 41-54. 2. Kovalenko Y., Konakhovych H., Kozlyuk I. (2020) Specificity of optimization of performance indicators of technical operation and updating of radio electronic systems of aircraft. International Journal of Engineering Research and Applications (IJERA), vol. 10 (09), pp. 48-58. 3. Kozlyuk І., Kovalenko Y. (2020) Functional bases of the software devel

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DiBenedetto, Michael F. "Citing criteria for the microwave landing system (MLS) MLS/ILS collocation and runway hump shadowing." Ohio : Ohio University, 1988. http://www.ohiolink.edu/etd/view.cgi?ohiou1182785020.

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Sprague, Kara Lynn 1980. "Design and validation of an avionics system for a miniature acrobatic helicopter." Thesis, Massachusetts Institute of Technology, 2002. http://hdl.handle.net/1721.1/87835.

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Thesis (M.Eng.)--Massachusetts Institute of Technology, Dept. of Electrical Engineering and Computer Science, 2002.<br>Includes bibliographical references (leaves 53-54).<br>by Kara Lynn Sprague.<br>M.Eng.

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Teng, Choon Hon Adrian. "Design and performance evaluation study of a prototype of a tactical unmanned aerial vehicle." Thesis, Monterey, Calif. : Naval Postgraduate School, 2007. http://bosun.nps.edu/uhtbin/hyperion-image.exe/07Dec%5FTeng.pdf.

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Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, December 2007.<br>Thesis Advisor(s): Jones, Kevin D. ; Dobrokhodov, Vladimir N. "December 2007." Description based on title screen as viewed on January 18, 2008. Includes bibliographical references (p. 97-98). Also available in print.

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Silva, Leon M. (Leon Manuel) 1968. "A partitioning methodology for helicopter avionics system with a focus on life cycle cost." Thesis, Massachusetts Institute of Technology, 2001. http://hdl.handle.net/1721.1/82690.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design & Management Program, 2001.<br>This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.<br>Includes bibliographical references (p. 111).<br>by Leon M. Silva.<br>S.M.

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Johansson, Viktor, and Alexander Vallén. "Random testing with sanitizers to detect concurrency bugs in embedded avionics software." Thesis, Linköpings universitet, Programvara och system, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-153310.

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Fuzz testing is a random testing technique that is effective at finding bugs in large software programs and protocols. We investigate if the technology can be used to find bugs in multi-threaded applications by fuzzing a real-time embedded avionics platform together with a tool specialized at finding data races between multiple threads. We choose to fuzz an API (available to applications executing on top) of the platform. This thesis evaluates aspects of integrating a fuzzing program, AFL and a sanitizer, ThreadSanitizer with an embedded system. We investigate the modifications needed to creat

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