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Artykuły w czasopismach na temat "Avionics"
Sun, Yi Gang, i Li Sun. "The Design of Avionics System Interfaces Emulation and Verification Platform Based on QAR Data". Applied Mechanics and Materials 668-669 (październik 2014): 879–83. http://dx.doi.org/10.4028/www.scientific.net/amm.668-669.879.
Pełny tekst źródłaSahputra, Afandi, Abdul Rasyid i Dika Aprillia. "Pemanfaatan Automatic Direction Finder KR87 Pada Avionics System Trainer AT-01 Untuk Meningkatkan Kompetensi Lulusan SMK Penerbangan". TRIDARMA: Pengabdian Kepada Masyarakat (PkM) 5, nr 1 (30.05.2022): 272–81. http://dx.doi.org/10.35335/abdimas.v5i1.2513.
Pełny tekst źródłaNadesakumar, A., R. M. Crowder i 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, nr 4 (grudzień 1995): 265–72. http://dx.doi.org/10.1243/pime_proc_1995_209_300_02.
Pełny tekst źródłaHuang, Jin, Bo Xu i Kun Qiu. "Modeling and Simulation of FC-AE-ASM Network". Advanced Materials Research 748 (sierpień 2013): 941–45. http://dx.doi.org/10.4028/www.scientific.net/amr.748.941.
Pełny tekst źródłaWang, Ying, Jian Yong Wang i Lei Wang. "A Transformation-Based Integrated Modular Avionics Software Model Construction Approach". Applied Mechanics and Materials 668-669 (październik 2014): 343–46. http://dx.doi.org/10.4028/www.scientific.net/amm.668-669.343.
Pełny tekst źródłaZhang, Jian Dong, En Long Cao, Yong Wu i Guo Qing Shi. "Designing and Realizing of Universal Test and Analysis System of Avionics Data Bus". Applied Mechanics and Materials 284-287 (styczeń 2013): 2371–74. http://dx.doi.org/10.4028/www.scientific.net/amm.284-287.2371.
Pełny tekst źródłaJiang, Na, Chunpeng Zhang, Yang Cao i Rixin Zhan. "Application of prognostic and health management in avionics system". Highlights in Science, Engineering and Technology 7 (3.08.2022): 1–9. http://dx.doi.org/10.54097/hset.v7i.988.
Pełny tekst źródłaZieja, Mariusz, Andrzej Szelmanowski, Andrzej Pazur i Grzegorz Kowalczyk. "Computer Life-Cycle Management System for Avionics Software as a Tool for Supporting the Sustainable Development of Air Transport". Sustainability 13, nr 3 (2.02.2021): 1547. http://dx.doi.org/10.3390/su13031547.
Pełny tekst źródłaGuryanov, A. V. "RESSEARCH OF VARIANTS FOR ORGANIZING THE SUPPLY CHAIN OF AVIONIC EQUIPMENT TO MAINTAIN THE SERVICEABILITY OF AVIONICS OBJECTS". System analysis and logistics 4, nr 30 (22.12.2021): 106–13. http://dx.doi.org/10.31799/2077-5687-2021-4-106-113.
Pełny tekst źródłaZhang, Xiao-Jun. "Research on Anti-saturation Feedback Control Method for UAV Avionics System". MATEC Web of Conferences 232 (2018): 04008. http://dx.doi.org/10.1051/matecconf/201823204008.
Pełny tekst źródłaRozprawy doktorskie na temat "Avionics"
Omiecinski, Tomasz Adam. "Reconfigurable integrated modular avionics". Thesis, University of Bristol, 1999. http://hdl.handle.net/1983/e9e10bd7-72c6-4aff-9027-f297dded5e41.
Pełny tekst źródłaPyatrin, D. K., O. V. Kozhokhina, G. Y. Marinchenko, L. V. Blahaia, Д. К. Пятрін, О. В. Кожохіна, Г. Є. Марінченко i Л. В. Благая. "Weibull distribution avionics application". Thesis, National aviation university, 2021. https://er.nau.edu.ua/handle/NAU/50499.
Pełny tekst źródłaThe paper deals with the weibull distribution in avionics application. During the operation of aircraft, the events that determine the transition of the product to different technical states occur randomly. Intervals of time of stay of a product in this or that condition have casual values of duration. The Weibull distribution is a fairly flexible function that can well align a variety of failure statistics and can be a model for the reliability of both electronic and mechanical products. The Weibull distribution successfully can be used in reliability engineering and failure analysis.
У тезах розглядається розподіл Вейбулла в застосуванні до авіоніки. Під час експлуатації літальних апаратів події, що визначають перехід виробу в різні технічні стани, відбуваються випадковим чином. Інтервали часу перебування виробу в тому чи іншому стані мають випадкові значення тривалості. Розподіл Вейбулла — це досить гнучка функція, яка може добре узгоджувати різноманітні статистичні дані про відмови та може бути взірцем надійності як електронних, так і механічних виробів. Розподіл Вейбулла може бути використаний в прогнозуванні надійності авіоніки та аналізі відмов.
Tybrandt, Ola. "Distribution of Cooling to Avionics". Thesis, Linköpings universitet, Reglerteknik, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-79031.
Pełny tekst źródłaCzerwonka, Stephen P. (Stephen Paul) 1976. "Avionics life-cycle forecasting model". Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/9242.
Pełny tekst źródłaAlso available online at the MIT Theses Online homepage
Includes bibliographical references (p. 116-119).
by Stephen P. Czerwonka.
S.M.
Sukardjo, Wishnu. "Methods of avionics systems maintenance procedures". Thesis, University of Central Lancashire, 1995. http://clok.uclan.ac.uk/21166/.
Pełny tekst źródłaByrne, James Michael Jr. "Resource-constrained avionics design for CubeSats". Thesis, Massachusetts Institute of Technology, 2016. http://hdl.handle.net/1721.1/105559.
Pełny tekst źródłaThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
Cataloged from student-submitted PDF version of thesis.
Includes bibliographical references (pages 90-92).
We present an optimization approach to CubeSat avionics design which considers the consumption of some resources (electrical power, volume) and production of others (processing power, volatile memory, non-volatile memory, and radiation tolerance) in a quantitative optimization analysis. We present the avionics hardware design for the Microwave Radiometer Technology Acceleration (MiRaTA) 3U CubeSat, funded by the NASA Earth Science Technology Office (ESTO), as a case study for our optimization analysis. MiRaTA will demonstrate a three-band microwave radiometer and GPS radio occultation (GPSRO) sensor suite for profiling atmospheric temperature, humidity, and cloud ice. The goal is to increase the Technology Readiness Level (TRL) of the weather-sensing technology from TRL 5 to TRL 71. The avionics system is the "central nervous system" of the spacecraft, managing interfaces with every subsystem and between the Bus and Payload. MiRaTA's avionics design supports the Payload, which is tasked with the science mission to gather and process appropriate radiometer and GPSRO data, and the Bus, which comprises subsystems to handle attitude determination and control (ADC), power regulation and distribution, communications with the ground station, thermal management, and a suite of sensors and telemetry components. MiRaTA's avionics system uses a custom designed motherboard with a PIC24FJ256GB210 microcontroller to command activity in the Bus and manage data and power for the Payload. This custom Motherboard - dubbed the "Micron Motherboard" - leverages many of the advantages of the popular Pumpkin Motherboard but with reduced complexity and improved performance. The MiRaTA avionics system is also designed to minimize the number and length of cables, simplify connector uniformity, and improve accessibility. The design improvement in avionics hardware from MicroMAS to MiRaTA is quantified using an optimization coefficient: 1.522. We expect optimization coefficients to range typically from -4 to +4, so this design indicates a modest improvement.
by James Michael Byrne, Jr.
S.M.
Warden, Gary, i Bill Fleissner. "FIBRE CHANNEL TESTING FOR AVIONICS APPLICATIONS". International Foundation for Telemetering, 2004. http://hdl.handle.net/10150/605804.
Pełny tekst źródłaFibre Channel is being implemented as an avionics communication architecture for a variety of new military aircraft and upgrades to existing aircraft. The Fibre Channel standard (see T11 web site www.t11.org) defines various network topologies and multiple data protocols. Some of the topologies and protocols (ASM, 1553, RDMA) are suited for Avionics applications, where the movement of data between devices must take place in a deterministic fashion and needs to be delivered very reliably. All aircraft flight hardware needs to be tested to be sure that it will communicate information properly in the Fibre Channel network. The airframe manufacture needs to test the integrated network to verify that all flight hardware is communicating properly. Continuous maintenance testing is required to insure that all communication is deterministic and reliable. This paper provides an overview of a Fibre Channel Avionics network and protocols being used for Avionics. The paper also discusses a practical implementation of avionics level testing and testing challenges associated with these applications.
Gavrilets, Vladislav 1975. "Avionics systems development for small unmanned aircraft". Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/50382.
Pełny tekst źródłaBuckley, Dave. "New Monitoring Paradigms for Modern Avionics Buses". International Foundation for Telemetering, 2013. http://hdl.handle.net/10150/579530.
Pełny tekst źródłaIn modern aircraft there is a proliferation of avionics buses. Some of these buses use industry wide standards such as ARINC 429 or AFDX while others are based on proprietary protocols. For many of the newer bus types there can be thousands of parameters on each bus. In a distributed data acquisition system the flight test engineer needs to record all of the data from each bus and monitor selected parameters in real time. There are numerous different approaches to acquiring, transmitting and recording data from avionics buses. In modern FTI there is also a proliferation of standards for recording and transmission including IRIG 106 Chapter 10, iNET and IENA. In this paper some common approaches to bus monitoring are compared and contrasted for popular buses such as ARINC 429, AFDX and Time Triggered Protocol. For each bus type the best approach is selected for reliable acquisition, speed of configuration, low latency telemetry and compact recording which is optimized for playback.
Black, James A. "HIGH SPEED AVIONICS DATA INSTRUMENTATION SYSTEM (HADIS)". International Foundation for Telemetering, 1992. http://hdl.handle.net/10150/608905.
Pełny tekst źródłaSAIC, 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, and its ability to rapidly reconfigure its interfaces based on field programmable gate arrays. The paper discusses the need for multiple data paths within the system to allow parallel operations to take place, the need for dedicated access to the recorder subsystem, and methods for allowing selective recording based on the information content of the data. The effort was sponsored by the Test Facility Working Group to provide a common data collection system for Air Force logistics and test and evaluation facilities. The design is owned by the government and may be cost-effectively used by any government agency.
Książki na temat "Avionics"
), Brinkman David (Ed, red. Jane's Avionics. Coulsdon: Jane's Information Group, 1995.
Znajdź pełny tekst źródłainc, United Air Lines, red. Avionics fundamentals. Casper, WY: IAP, Inc., 1991.
Znajdź pełny tekst źródłaCollinson, R. P. G., red. Introduction to Avionics. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6.
Pełny tekst źródłaMoir, Ian, i Allan G. Seabridge. Military Avionics Systems. Chichester, UK: John Wiley & Sons, Ltd, 2006. http://dx.doi.org/10.1002/0470035463.
Pełny tekst źródłaMoir, Ian, Allan Seabridge i Malcolm Jukes. Civil Avionics Systems. Chichester, UK: John Wiley & Sons, Ltd, 2013. http://dx.doi.org/10.1002/9781118536704.
Pełny tekst źródłaKayton, Myron, i Walter R. Fried, red. Avionics Navigation Systems. Hoboken, NJ, USA: John Wiley & Sons, Inc., 1997. http://dx.doi.org/10.1002/9780470172704.
Pełny tekst źródłaCollinson, R. P. G. Introduction to avionics. London: New York, 1996.
Znajdź pełny tekst źródłaMalcolm, Jukes, red. Military avionics systems. Hoboken, NJ: John Wiley & Sons, 2006.
Znajdź pełny tekst źródłaSeabridge, A. G. (Allan G.) i Jukes Malcolm, red. Civil avionics systems. Chichester, West Sussex: Wiley, 2013.
Znajdź pełny tekst źródłaMoir, I. Military avionics systems. Chichester, England: John Wiley & Sons Ltd., 2006.
Znajdź pełny tekst źródłaCzęści książek na temat "Avionics"
Weik, Martin H. "avionics". W Computer Science and Communications Dictionary, 93. Boston, MA: Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_1210.
Pełny tekst źródłaSarma, Kalluri R., Steve Grothe i Aaron Gannon. "Avionics Displays". W Handbook of Visual Display Technology, 253–74. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-14346-0_168.
Pełny tekst źródłaSarma, Kalluri R., Steve Grothe i Aaron Gannon. "Avionics Displays". W Handbook of Visual Display Technology, 1–17. Berlin, Heidelberg: Springer Berlin Heidelberg, 2015. http://dx.doi.org/10.1007/978-3-642-35947-7_168-1.
Pełny tekst źródłaWeik, Martin H. "avionics architecture". W Computer Science and Communications Dictionary, 93. Boston, MA: Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_1211.
Pełny tekst źródłaCollinson, R. P. G. "Avionics systems integration". W Introduction to Avionics, 406–30. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_9.
Pełny tekst źródłaCollinson, R. P. G. "Avionics Systems Integration". W Introduction to Avionics Systems, 459–87. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-0708-5_9.
Pełny tekst źródłaCollinson, R. P. G. "Avionics Systems Integration". W Introduction to Avionics Systems, 433–58. Boston, MA: Springer US, 2003. http://dx.doi.org/10.1007/978-1-4419-7466-2_9.
Pełny tekst źródłaWeik, Martin H. "open avionics architecture". W Computer Science and Communications Dictionary, 1143. Boston, MA: Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_12805.
Pełny tekst źródłaWeik, Martin H. "integrated modular avionics". W Computer Science and Communications Dictionary, 801. Boston, MA: Springer US, 2000. http://dx.doi.org/10.1007/1-4020-0613-6_9228.
Pełny tekst źródłaReichel, Reinhard. "Integrated avionics architectures". W Proceedings, 921. Wiesbaden: Springer Fachmedien Wiesbaden, 2019. http://dx.doi.org/10.1007/978-3-658-25939-6_71.
Pełny tekst źródłaStreszczenia konferencji na temat "Avionics"
Watkins, Mike, i Doug Garrette. "Advancing airlift avionics - C-17 avionics suite". W Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-986.
Pełny tekst źródłaWATKINS, MIKE, i DOUG GARRETTE. "Advancing airlift avionics - C-17 avionics suite". W Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1243.
Pełny tekst źródłaShibata, Minoru, i Haruo Notoh. "Avionics simulator". W Aerospace/Defense Sensing and Controls, redaktor Robert Lee Murrer, Jr. SPIE, 1996. http://dx.doi.org/10.1117/12.241115.
Pełny tekst źródłaVanderLeest, Steven H. "Avionics Linux". W 2023 IEEE/AIAA 42nd Digital Avionics Systems Conference (DASC). IEEE, 2023. http://dx.doi.org/10.1109/dasc58513.2023.10311247.
Pełny tekst źródłaWatkins, Christopher B., i Randy Walter. "Transitioning from federated avionics architectures to Integrated Modular Avionics". W 2007 IEEE/AIAA 26th Digital Avionics Systems Conference. IEEE, 2007. http://dx.doi.org/10.1109/dasc.2007.4391842.
Pełny tekst źródłaSamraj, Selvadhas. "Avionics systems integration using avionics full duplex swithched ethernet". W 2007 IEEE/AIAA 26th Digital Avionics Systems Conference. IEEE, 2007. http://dx.doi.org/10.1109/dasc.2007.4391867.
Pełny tekst źródłaZheng Li, Qiao Li i Huagang Xiong. "Avionics clouds: A generic scheme for future avionics systems". W 2012 IEEE/AIAA 31st Digital Avionics Systems Conference (DASC). IEEE, 2012. http://dx.doi.org/10.1109/dasc.2012.6382402.
Pełny tekst źródłaZheng Li. "Avionics clouds: A generic scheme for future avionics systems". W 2012 IEEE/AIAA 31st Digital Avionics Systems Conference (DASC). IEEE, 2012. http://dx.doi.org/10.1109/dasc.2012.6383082.
Pełny tekst źródłaDandekar, A. J., i L. E. Farhner. "Avionics Display Systems". W Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1988. http://dx.doi.org/10.4271/881371.
Pełny tekst źródłaMORRISON, R., i JON SIMMONS. "Advanced avionics interconnection". W Digital Avionics Systems Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3856.
Pełny tekst źródłaRaporty organizacyjne na temat "Avionics"
Bedzyk, William L., Donald R. Czech, Thomas J. Dickman, Frank S. Gruber, John F. Myers i John F. Myers. Advanced Avionics System Analysis. Modular Avionics Cost Benefit Study Formulation. Fort Belvoir, VA: Defense Technical Information Center, luty 1987. http://dx.doi.org/10.21236/ada189019.
Pełny tekst źródłaNAVAL AIR SYSTEMS COMMAND ARLINGTON VA. Advanced Avionics Architecture and Technology Review. Executive Summary and Volume 1, Avionics Technology. Volume 2. Avionics Systems Engineering. Fort Belvoir, VA: Defense Technical Information Center, sierpień 1993. http://dx.doi.org/10.21236/ada273630.
Pełny tekst źródłaRisko, Theodore. Avionics Diagnostic System (ADS). Fort Belvoir, VA: Defense Technical Information Center, czerwiec 1999. http://dx.doi.org/10.21236/ada368423.
Pełny tekst źródłaKellog, David L., J. K. Henderson, Mike J. Harris i Anthony J. Schiavone. Core Avionics and Standardization. Fort Belvoir, VA: Defense Technical Information Center, marzec 1992. http://dx.doi.org/10.21236/ada248326.
Pełny tekst źródłaDamania, Bhavesh, Steve Vestal, Devesh Bhatt i Rashmi Bhatt. Avionics System Performance Management. Fort Belvoir, VA: Defense Technical Information Center, maj 1998. http://dx.doi.org/10.21236/ada388145.
Pełny tekst źródłaNATIONAL RESEARCH COUNCIL WASHINGTON DC. Aging Avionics in Military Aircraft. Fort Belvoir, VA: Defense Technical Information Center, maj 2001. http://dx.doi.org/10.21236/ada397119.
Pełny tekst źródłaHavey, G., S. Lewis i G. Seifert. Avionics/Electronics Quick Reliability Assessment. Fort Belvoir, VA: Defense Technical Information Center, marzec 1998. http://dx.doi.org/10.21236/ada342681.
Pełny tekst źródłaGuiliano, John E. Rapid Avionics Test Modification Capability. Fort Belvoir, VA: Defense Technical Information Center, październik 1999. http://dx.doi.org/10.21236/ada388094.
Pełny tekst źródłaJones, Sid. Fibre Channel Avionics Bus Monitor. Fort Belvoir, VA: Defense Technical Information Center, luty 2001. http://dx.doi.org/10.21236/ada389673.
Pełny tekst źródłaAndrews, Robert B. Networked Avionics Part Task Trainer. Fort Belvoir, VA: Defense Technical Information Center, czerwiec 2000. http://dx.doi.org/10.21236/ada378377.
Pełny tekst źródła