Relevant bibliographies by topics / Avionic systems

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Avionic systems'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 May 2024

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Journal articles on the topic "Avionic systems"

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Sun, Yi Gang, and Li Sun. "The Design of Avionics System Interfaces Emulation and Verification Platform Based on QAR Data." Applied Mechanics and Materials 668-669 (October 2014): 879–83. http://dx.doi.org/10.4028/www.scientific.net/amm.668-669.879.

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In order to avoid the complex mathematical modeling and ensure the reliability of avionics system verification, this paper has designed an interfaces emulation and verification platform of avionics system based on QAR data. Platform includes 2 parts: Emulator and Simulator. Simulator generates the flight environmental data which is come from QAR and transforms the data into excitation signal of devices. Emulator emulates the interface features of avionic devices according to the ICD and can be replaced with real devices. By comparing the actual input-output data of devices with QAR theoretical
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Nadesakumar, A., R. M. Crowder, and C. J. Harris. "Advanced System Concepts for Future Civil Aircraft—an Overview of Avionic Architectures." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 209, no. 4 (1995): 265–72. http://dx.doi.org/10.1243/pime_proc_1995_209_300_02.

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The avionics systems of state-of-the-art commercial aircraft have become increasingly complex and sophisticated, in order to meet the ever increasing performance and reliability requirements. With the capability of the avionics technology improving by an order of magnitude every few years, it is envisaged that the current philosophy of one box-per-function will soon reach its limits in terms of cost, functionality, reliability, and certification. The proposed solution is the integrated systems configuration, using distributed processing, where the computational resources are shared between man
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Dove, Billy L. "Validation Methods for Programmable Avionic Systems." Safety and Reliability 6, no. 3 (1986): 7–17. http://dx.doi.org/10.1080/09617353.1986.11691130.

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Huang, Jin, Bo Xu, and Kun Qiu. "Modeling and Simulation of FC-AE-ASM Network." Advanced Materials Research 748 (August 2013): 941–45. http://dx.doi.org/10.4028/www.scientific.net/amr.748.941.

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Fibre Channel (FC) as a Universal Avionics Network (UAN) candidate solution for the advanced integrated avionics systems can enable high-bandwidth, low-latency, high-reliability and hard real-time communication on aircraft platforms spanning military and commercial applications. Fibre Channel Avionics Environment-Anonymous Subscriber Messaging protocol (FC-AE-ASM) is one of the five high level protocols in fiber channel avionic environment which is used to transport command, control, signal processing and sensor / video data of the aircraft[1,2].The objective of this paper is to conduct a mode
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Burger, Stefan, and Oliver Hummel. "Lessons Learnt from Gauging Software Metrics of Cabin Software in a Commercial Airliner." ISRN Software Engineering 2012 (October 15, 2012): 1–11. http://dx.doi.org/10.5402/2012/162305.

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In order to achieve high safety standards, avionic software needs to be developed with very high requirements regarding safety, reliability, and determinism as well as real-time constraints, which are often in conflict with the development of maintainable software systems. Nevertheless, the ability to change the software of an airplane is of increasing importance, since it consists of a multitude of partially hardware-specific subsystems which may need replacement during a plane’s lifespan of typically numerous decades. Thus, as a first step towards optimizing maintainability of avionic softwa
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Aakash, Kislaya, Armaan Aditya, and G. Srinivas. "Recent Developments of Modern Avionic Systems in Aeronautical Applications." Journal of Advanced Research in Dynamical and Control Systems 11, no. 12-SPECIAL ISSUE (2019): 923–29. http://dx.doi.org/10.5373/jardcs/v11sp12/20193294.

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Jastrzębski, Grzegorz, Paweł Szczepaniak, and Michał Jóźko. "Issues Related To Troubleshooting Of Avionic Hydraulic Units." Journal of KONBiN 30, no. 1 (2014): 59–73. http://dx.doi.org/10.2478/jok-2014-0015.

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Abstract The paper outlines workflows associated with troubleshooting of avionic hydraulic systems with detailed description of the troubleshooting algorithm and classification of diagnostic signals provided by avionic hydraulic systems and their subassemblies. Attention is paid to measurement sequences for diagnostic signals from hydraulic systems, circuits and units. Detailed description is dedicated to an innovative design of a troubleshooting device intended for direct measurements of internal leaks from avionic hydraulic units. Advantages of the proposed measurement method are summarized
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Zhang, Jian Dong, En Long Cao, Yong Wu, and Guo Qing Shi. "Designing and Realizing of Universal Test and Analysis System of Avionics Data Bus." Applied Mechanics and Materials 284-287 (January 2013): 2371–74. http://dx.doi.org/10.4028/www.scientific.net/amm.284-287.2371.

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In modern combat aircrafts, avionics integrated systems play an increasingly important role. Bus test and analysis system is used as a testing platform for the testing, debugging, maintenance and monitoring of airborne electronic equipment, which could rapidly detect and identify the working status of the bus. This paper discusses the general avionics data bus test system design and implementation, which focuses on the test system design, system management, software development, and the bus information flow management of the whole system. The universal test and analysis system is based on the
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Banerjee, P. Pat, David He, Shenliang Wu, and Eric Bechhoefer. "Discriminant Analysis Based Prognostics of Avionic Systems." IEEE Transactions on Systems, Man, and Cybernetics, Part C (Applications and Reviews) 37, no. 6 (2007): 1318–26. http://dx.doi.org/10.1109/tsmcc.2007.905838.

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Johar, Harminder Singh, Abhijit Bhattacharyya, and Srinivas Rao S. "Fault Tolerant Power Supply for Aircraft Store Interface." Defence Science Journal 72, no. 5 (2022): 679–86. http://dx.doi.org/10.14429/dsj.72.17737.

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This paper brings out the design of a fault-tolerant power supply unit for the aircraft-store interface. This switched mode power supply provides multiple 30 V regulated and isolated DC outputs required for pre-launch preparations and auto-launch operations of avionic sub-systems in a store. 3Ø-115V-400Hz-AC supply as well as 27V-DC supply are available from a fighter aircraft for powering up of any store. Power (wattage) output from 27V/10A DC is inadequate to power up various onboard avionic sub-systems in guided stores involving seekers and other avionics. Hence, it is planned to convert av
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Dissertations / Theses on the topic "Avionic systems"

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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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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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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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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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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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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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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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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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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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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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Books on the topic "Avionic systems"

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1921-, Middleton Don, ed. Avionic systems. Longman Scientific & Technical, 1989.

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Avionic systems design. CRC Press, 1994.

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Avionic systems: Operation & maintenance. IAP, 1993.

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Aerospace, Avionic Systems Division Conference (3rd 1993 Denver Colorado). 1993 Aerospace Avionic Systems Division Conference proceedings. Society of Automotive Engineers, 1993.

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Engineers, Institution of Mechanical, Royal Aeronautical Society, and Institution of Electrical Engineers, eds. Avionic systems, design, and software: Selected papers from Aerotech 95. Mechanical Engineering Publications Limited for The Institution of Mechanical Engineers, 1996.

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service), SpringerLink (Online, ed. Energy Efficient Microwave Systems: Materials Processing Technologies for Avionic, Mobility and Environmental Applications. Springer-Verlag Berlin Heidelberg, 2009.

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Center, Langley Research, ed. Investigation of RF emissions from wireless networks as a threat to avionic systems. National Aeronautics and Space Administration, Langley Research Center, 2002.

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M, Assenheim H., Society of Photo-optical Instrumentation Engineers., IS & T--the Society for Imaging Science and Technology., and Rochester Institute of Technology. Center for Imaging Science., eds. Large-screen-projection, avionic, and helmet-mounted displays: 26-28 February 1991, San Jose, California. SPIE, 1991.

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Society, Royal Aeronautical, ed. Cost-effective avionic and weapon systems: Spring convention 14th and 15th May 1986 : proceedings. Royal Aeronautical Society, 1986.

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Society, Royal Aeronautical, ed. Avionic systems/design and maintenance: Proceedings [of a one day conference] Thursday 22 April 1993. Royal Aeronautical Society, 1993.

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Book chapters on the topic "Avionic systems"

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Tooley, Mike. "Avionic Systems." In Aircraft Digital Electronic and Computer Systems, 3rd ed. Routledge, 2022. http://dx.doi.org/10.1201/9781003215516-15.

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Cebrián, David, Valentín Valero, and Fernando Cuartero. "Automation of Avionic Systems Testing." In Testing of Software and Communicating Systems. Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-73066-8_3.

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Chen, Wen. "Advances in Integrated Avionic Systems." In Proceedings of the 2022 3rd International Conference on Artificial Intelligence and Education (IC-ICAIE 2022). Atlantis Press International BV, 2023. http://dx.doi.org/10.2991/978-94-6463-040-4_239.

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Feher, Lambert E. "Avionic Microwave Anti-/De-Icing Systems." In Energy Efficient Microwave Systems. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-92122-6_5.

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Larrieu, Nicolas, and Antoine Varet. "Methodology for Rapid Prototyping Avionic Software." In Rapid Prototyping of Software for Avionics Systems. John Wiley & Sons, Inc., 2014. http://dx.doi.org/10.1002/9781119050643.ch2.

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Bapp, Falco K., and Jürgen Becker. "Advances in Avionic Platforms: Multi-core Systems." In Advances in Aeronautical Informatics. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-75058-3_2.

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Feher, Lambert, and Manfred Thumm. "Design of Avionic Microwave De-/Anti-Icing Systems." In Advances in Microwave and Radio Frequency Processing. Springer Berlin Heidelberg, 2006. http://dx.doi.org/10.1007/978-3-540-32944-2_76.

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Rhouas, Imane, and Khalid Nafil. "Avionic Software and Agile Development: A Systematic Mapping Study." In Information Systems and Technologies. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-04819-7_6.

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Simani, Silvio, Paolo Castaldi, and Saverio Farsoni. "Fault Diagnosis and Fault-Tolerant Control for Avionic Systems." In Advances in Intelligent Systems and Computing. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-55180-3_16.

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Fernández, José L., and Juan A. De La Puente. "Constructing a pilot library of components for avionic systems." In Ada: The Choice for '92. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/bfb0018506.

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Conference papers on the topic "Avionic systems"

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Carbonari, Armando. "Avionic systems overview." In the 17th symposium. ACM Press, 2004. http://dx.doi.org/10.1145/1016568.1016570.

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Cai, Steve Q., Avijit Bhunia, and Julie Asfia. "A Combined Heat Pipe Solution for Long Distance Thermal Management." In ASME 2016 Heat Transfer Summer Conference collocated with the ASME 2016 Fluids Engineering Division Summer Meeting and the ASME 2016 14th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/ht2016-7342.

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A heat pipe can efficiently transfer heat through it liquid-vapor phase change mechanism. Among different heat pipes, loop heat pipe (LHP) and pulsating heat pipe (PHP) are known to be capable of high heat flux/high load heat transfer. In this article, LHP and PHP heat transfer systems are combined to achieve passive, reliable and long-distance heat transfer for successful thermal management of modern avionic systems. Aiming at this development goal, a 2m long LHP is designed to transport heat from the avionics chassis to the remote heat rejection site. To reduce saturation pressure and ensure
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JANEX, ALBERT. "Reflections on avionic integration." In Digital Avionics Systems Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3950.

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Vergnolle, Claude, and Bruno Houssay. "Interconnection requirements in avionic systems." In Fibers '91, Boston, MA, edited by Gnanalingam Arjavalingam and James Pazaris. SPIE, 1991. http://dx.doi.org/10.1117/12.25566.

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Abbas, Gregory L., Chi-Shain Hong, Raymond W. Huggins, et al. "Photonics technology for avionic systems." In OE/LASE '94, edited by Pei C. Chen, Lawrence A. Johnson, and Henryk Temkin. SPIE, 1994. http://dx.doi.org/10.1117/12.176625.

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Casazza, Jeffrey. "Mixed Voltage, Microprocessor Based Avionic Systems." In Aerospace Technology Conference and Exposition. SAE International, 1995. http://dx.doi.org/10.4271/952028.

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Audsley, N. C., A. Grigg, M. Fletcher, and A. Wake. "Portable code in future avionic systems." In IEE Colloquium on Real-Time Systems. IEE, 1998. http://dx.doi.org/10.1049/ic:19980524.

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Heydari, Vahid. "Moving Target Defense for Avionic Systems." In 2018 National Cyber Summit (NCS). IEEE, 2018. http://dx.doi.org/10.1109/ncs.2018.00013.

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Richards, Mark A. "The Rapid Prototyping of Application Specific Signal Processor (RASSP) Program: Overview and Accomplishments." In Avionic Systems Division Meeting. SAE International, 1994. http://dx.doi.org/10.4271/942550.

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Christiano, Paul F., and Brent E. Moats. "Time Domain Design/Analysis Tool for the MIL-STD-1553B Data Bus." In Avionic Systems Division Meeting. SAE International, 1994. http://dx.doi.org/10.4271/942551.

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Reports on the topic "Avionic systems"

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Sotello, Wendy J., John T. Penner, Cynthia K. Scharf, and James B. Keeth. F-16 Avionic Systems Attack Control, Instrument and Flight Control, Communication, Navigation, and Penetration Aids. Training Requirements Analysis 452X2. Volume 1. Defense Technical Information Center, 1992. http://dx.doi.org/10.21236/ada252786.

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Risko, Theodore. Avionics Diagnostic System (ADS). Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada368423.

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Damania, Bhavesh, Steve Vestal, Devesh Bhatt, and Rashmi Bhatt. Avionics System Performance Management. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada388145.

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Bedzyk, William L., Donald R. Czech, Thomas J. Dickman, Frank S. Gruber, John F. Myers, and John F. Myers. Advanced Avionics System Analysis. Modular Avionics Cost Benefit Study Formulation. Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada189019.

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Satterthwaite, Charles P. Technologies for Avionics Embedded Computer Systems. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada276364.

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Reeve, Tammy. Pitfalls of Designing, Developing, and Maintaining Modular Avionics Systems in the Name of Sustainability. SAE International, 2024. http://dx.doi.org/10.4271/epr2024010.

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&lt;div class="section abstract"&gt;&lt;div class="htmlview paragraph"&gt;Sustainability is both an ethical responsibility and business concern for the aerospace industry. Military and commercial avionics developers have pushed toward a common standard for interfaces, computing platforms, and software in hopes of having “reusability” and reducing weight with backplane computing architectures which, in theory, would support commonality across aircraft systems. The integrated modular avionics (IMA) and military Future Airborne Capability Environment (FACE) standards are two such examples. They e
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NAVAL AIR SYSTEMS COMMAND ARLINGTON VA. Advanced Avionics Architecture and Technology Review. Executive Summary and Volume 1, Avionics Technology. Volume 2. Avionics Systems Engineering. Defense Technical Information Center, 1993. http://dx.doi.org/10.21236/ada273630.

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AIR FORCE TEST PILOT SCHOOL EDWARDS AFB CA. Volume III. Systems Phase, Chapter 7: Integrated Avionics Systems. Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada320032.

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Lucka, Doug, and Bill Michael. A Comprehensive Approach to Teaching Avionics Systems Flight Test. Defense Technical Information Center, 1999. http://dx.doi.org/10.21236/ada368650.

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Orsagh, Rolf, Douglas Brown, Michael Roemer, Thomas Dabney, and Andrew Hess. Prognostic Health Management for Avionics System Power Supplies. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada448885.

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