Relevant bibliographies by topics / Avionický systém

Contents

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

Academic literature on the topic 'Avionický systém'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Avionický systém"

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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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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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Zieja, Mariusz, Andrzej Szelmanowski, Andrzej Pazur, and Grzegorz Kowalczyk. "Computer Life-Cycle Management System for Avionics Software as a Tool for Supporting the Sustainable Development of Air Transport." Sustainability 13, no. 3 (2021): 1547. http://dx.doi.org/10.3390/su13031547.

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The article presents selected results of analytical and design works undertaken at the Air Force Institute of Technology (AFIT) in the field of building a computer support and software lifecycle management system that is critical for flight safety. The aim of the work undertaken is to develop methods and carry out verification and testing in order to detect errors in the developed avionics software for compliance with the requirements of the DO-178C standard and its production, certification, and implementation on board aircraft. The authors developed an original computer system within the imp
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Wang, Ying, and Lei Wang. "Automatic C Code Generation for Avionics Software Based on VxWorks653 Platform." Applied Mechanics and Materials 687-691 (November 2014): 3124–27. http://dx.doi.org/10.4028/www.scientific.net/amm.687-691.3124.

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At present, model-driven development method has been gradually applied in safety-critical avionics software to improve reliability and productivity. Existing ARINC653 annex of the Architecture Analysis & Design Language (AADL) is used to model avionic software based on ARINC653-compatible OS, such as VxWorks653 commercial platform. In this paper, a refined C code generation algorithm is proposed to enable automatically generate VxWorks653-runnable code from the AADL ARINC653 models. Finally, a simplified autopilot system example is as a case study to show the validity of our approch.
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Ma, Teng Da, and De Xin Zhou. "Design of Civil Aircraft Avionics System Bus Excitation System." Advanced Materials Research 1037 (October 2014): 193–96. http://dx.doi.org/10.4028/www.scientific.net/amr.1037.193.

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The avionics system is a core component of the civil aircraft. To reduce the risk and cost of developing avionics system, shorten the development cycle, through the development process of avionics systems, variety of simulation and verification must be done. The bus excitation signals need to be provided for each avionics unit and the signals from each avionics unit need to be received and processed. The multilayer abstract model and organizational structure model of the bus excitation system was established. And a complete bus excitation system was designed. In this system, the ARINC429 bus s
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Dudziak, Jacek, and Paweł Guła. "Design practice in the translation traditional and glass cockpit based on General Aviation I-31T aircraft." Aircraft Engineering and Aerospace Technology 89, no. 6 (2017): 749–56. http://dx.doi.org/10.1108/aeat-04-2016-0058.

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Purpose The aim of this paper is to present the results preparation of a new glass cockpit for a general aviation category airplane with a TP100 turboprop 180 kW engine. All the works were carried out within the framework of the European programme: “Efficient Systems and Propulsion for Small Aircraft” – ESPOSA. Design/methodology/approach As a part of the ongoing work, the avionics equipment available on the market were thoroughly analysed. Optimization of choice was defined at the level of costs, ergonomics and development requirements of the engine manufacturer. The paper presents the issues
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Park, Han-Joon, Kwang-Chun Go, and Jae-Hyun Kim. "Design Method for Integrated Modular Avionics System Architecture." Journal of Korea Information and Communications Society 39C, no. 11 (2014): 1094–103. http://dx.doi.org/10.7840/kics.2014.39c.11.1094.

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Smith, Kevin M. "Mission Performance Aid for Aerial Combat." International Journal of Aviation Systems, Operations and Training 3, no. 1 (2016): 1–19. http://dx.doi.org/10.4018/ijasot.2016010101.

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This paper addresses the concepts, methods, apparatus, and tools used to establish the operational requirements and system architecture for an advanced mission performance aid (the smart cockpit) that targets aerial combat operations. As the complexity of our modern avionic systems increase, it is important to define operational requirements and crew station display features early in the design cycle. Many observers insist higher quality front-end work be performed to reduce the growing number of back-end mistakes and cost overruns. This paper provides a top-down orientation that treats platfo
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Ge, Xing Guo, Zhong Xiang Tao, and Chun Yan Tian. "Analysis of the Development Trend of Avionics System." Advanced Materials Research 850-851 (December 2013): 1102–5. http://dx.doi.org/10.4028/www.scientific.net/amr.850-851.1102.

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Avionics system has been existed for over 80 years and plays more and more important roles in the war today. The process of development of the avionics system in general and its modification are described. The technique performance and properties of several avionics system seekers are analyzed, and development trend of avionics system are discussed.
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Dissertations / Theses on the topic "Avionický systém"

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Vaňousová, Jana. "Koncepční návrh moderního avionického systému pro letoun kategorie EASA CS-23." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2018. http://www.nusl.cz/ntk/nusl-377481.

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This master thesis covers with the modern architecture of avionics system for EASA CS-23 AIRPL. The thesis contains EASA CS-23 and EU-OPS analysis and market analysis of avionics systems for this category of aircrafts. The thesis also includes the design of avionics system architecture and its safety and reliability assessment – used tool is Failure Mode and Effect Analysis (FMEA). At the end of the thesis there is assesment of potential attack of the avionics system by third part.
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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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Kadlčík, Jiří. "Celokovový letoun kategorie UL a LSA s aplikací moderních avionických, řídících a kontrolních systémů." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2011. http://www.nusl.cz/ntk/nusl-229451.

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This thesis is focused on a project of all metal aircraft by UL-2 and LSA rules. The background research of aircrafts in existing category has been made in the market. The concept, with whom this thesis deals with, has been projected thanks to this analysis. The second part of the thesis is focused on avionics equipments of aircrafts. Market analysis has been made and the way of medernizing small sports airfts' equipment in categories UL and LSA has been projected.
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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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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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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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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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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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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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Paquette, Jean J. R. Carleton University Dissertation Engineering Electrical. "The Next generation avionic system; a prediction." Ottawa, 1985.

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Books on the topic "Avionický systém"

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Hanaway, John F. Space shuttle avionics system. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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Moir, Ian. Military avionics systems. John Wiley & Sons, 2006.

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Spitzer, Cary R. Digital avionics systems. Prentice-Hall, 1987.

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G, Seabridge A., ed. Civil avionics systems. American Institute of Aeronautics and Astronautics, 2003.

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Seabridge, A. G. (Allan G.) and Jukes Malcolm, eds. Civil avionics systems. Wiley, 2013.

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Moir, Ian, and Allan G. Seabridge. Military Avionics Systems. John Wiley & Sons, Ltd, 2006. http://dx.doi.org/10.1002/0470035463.

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Moir, Ian, Allan Seabridge, and Malcolm Jukes. Civil Avionics Systems. John Wiley & Sons, Ltd, 2013. http://dx.doi.org/10.1002/9781118536704.

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Kayton, Myron, and Walter R. Fried, eds. Avionics Navigation Systems. John Wiley & Sons, Inc., 1997. http://dx.doi.org/10.1002/9780470172704.

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Moir, I. Military avionics systems. John Wiley & Sons Ltd., 2006.

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Malcolm, Jukes, ed. Military avionics systems. John Wiley & Sons, 2006.

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Book chapters on the topic "Avionický systém"

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Watson, Michael D., Kosta Varnavas, Clint Patrick, et al. "Avionics Health Management." In System Health Management. John Wiley & Sons, Ltd, 2011. http://dx.doi.org/10.1002/9781119994053.ch28.

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Collinson, R. P. G. "Avionics Systems Integration." In Introduction to Avionics Systems. Springer US, 2003. http://dx.doi.org/10.1007/978-1-4419-7466-2_9.

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Collinson, R. P. G. "Avionics systems integration." In Introduction to Avionics. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_9.

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Collinson, R. P. G. "Avionics Systems Integration." In Introduction to Avionics Systems. Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-0708-5_9.

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Collinson, R. P. G. "Navigation systems." In Introduction to Avionics. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_6.

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Collinson, R. P. G. "Inertial sensors and systems." In Introduction to Avionics. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_5.

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Collinson, R. P. G. "Navigation Systems." In Introduction to Avionics Systems. Springer US, 2003. http://dx.doi.org/10.1007/978-1-4419-7466-2_6.

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Collinson, R. P. G. "Navigation Systems." In Introduction to Avionics Systems. Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-0708-5_6.

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Collinson, R. P. G. "Autopilots and flight management systems." In Introduction to Avionics. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_8.

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Collinson, R. P. G. "Air data and air data systems." In Introduction to Avionics. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_2.

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Conference papers on the topic "Avionický systém"

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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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Patel, R. S., and C. E. Lents. "Optimal Thermal Management System for HALE UAV." In ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1991. http://dx.doi.org/10.1115/91-gt-396.

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This paper discusses an optimal thermal management system for a High Altitude Long Endurance Unmanned Air vehicle (HALE UAV). It examines several configurations to reject waste heat from the vehicle’s propulsion engine cooling system as well as the avionic cooling system and identifies the configuration which has a minimum impact on aircraft endurance, component reliability, and development risks. The optimization process incorporates two basic heat rejection approaches. One is a conventional approach which rejects cooling system waste heat to the atmosphere, and the other is a waste heat reco
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Pierce, David, and Justin Littlefield-Lawwill. "Information Assurance and Open Architecture Integrated Modular Avionics." In 2008 2nd Annual IEEE Systems Conference. IEEE, 2008. http://dx.doi.org/10.1109/systems.2008.4519034.

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Tokar, Joyce L. "Open System Architectures for Unmanned Avionics Systems." In 2018 AIAA Information Systems-AIAA Infotech @ Aerospace. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1459.

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Haider, Kamal, Jeffrey Tweedale, Pierre Urlings, and Lakhmi Jain. "Enhancing Avionics Systems Reliability and Maintainability through Development of IDSS - A Systems Approach." In 2008 2nd Annual IEEE Systems Conference. IEEE, 2008. http://dx.doi.org/10.1109/systems.2008.4519021.

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Bluff, R. J. "Avionic system modelling." In International Conference on Simulation (1998). IEE, 1998. http://dx.doi.org/10.1049/cp:19980610.

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Dandekar, A. J., and L. E. Farhner. "Avionics Display Systems." In Aerospace Technology Conference and Exposition. SAE International, 1988. http://dx.doi.org/10.4271/881371.

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Kulkarni, Chetan S., Gautam Biswas, Xenofon Koutsoukos, Jose Celaya, and Kai Goebel. "Diagnostic/Prognostic Experiments for Capacitor Degradation and Health Monitoring in DC-DC Converters." In ASME 2010 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. ASMEDC, 2010. http://dx.doi.org/10.1115/smasis2010-3862.

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Studying and analyzing the ageing mechanisms of electronic components avionics in systems such as the GPS and INAV are of critical importance. In DC-DC power converter systems electrolytic capacitors and MOSFET’s have higher failure rates among the components. Degradation in the capacitors under varying operating conditions leads to high ripples output voltages and currents affecting downstream components leading to cascading faults. For example, in avionics systems where the power supply drives a GPS unit, ripple currents can cause glitches in the GPS position and velocity output, and this ma
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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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Samraj, Selvadhas. "Avionics systems integration using avionics full duplex swithched ethernet." In 2007 IEEE/AIAA 26th Digital Avionics Systems Conference. IEEE, 2007. http://dx.doi.org/10.1109/dasc.2007.4391867.

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Reports on the topic "Avionický systém"

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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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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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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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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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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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Luckham, David C. Research into Development of Executable Reference Architectures for Avionics Systems. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada384505.

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Clemente, Paul, and John Bergey. The U.S. Army's Common Avionics Architecture System (CAAS) Product Line: A Case Study. Defense Technical Information Center, 2005. http://dx.doi.org/10.21236/ada444361.

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