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Dissertations / Theses on the topic 'Avionický systém'

Author: Grafiati

Published: 4 June 2021

Last updated: 1 February 2022

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1

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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2

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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3

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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4

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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5

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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6

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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7

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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8

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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9

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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10

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

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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

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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13

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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14

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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15

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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16

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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17

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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18

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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19

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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20

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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21

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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22

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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23

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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24

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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25

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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26

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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27

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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28

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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29

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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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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31

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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32

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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33

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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34

Mačišák, Lukáš. "Problematika testování a verifikace softwaru pro leteckou techniku." Master's thesis, Vysoké učení technické v Brně. Fakulta informačních technologií, 2011. http://www.nusl.cz/ntk/nusl-236942.

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This Master's Thesis describes methods of software certification and development of airborne systems, focusing on software testing and verification during project's life cycle. Thesis includes also designed software verification plan for concrete application according to RTCA/DO-178B. Another part of thesis illustrates the exemplary realization of tests according to designed verification plan. At the close we describe the options of applying the designed verification plan and evaluation of its results.

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35

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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36

Aab, Steven D. "Performance Analysis of the Local Area Augmentation System as the Position Sensor for the Runway Incursion Prevention System." Ohio University / OhioLINK, 2005. http://www.ohiolink.edu/etd/view.cgi?ohiou1121182284.

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37

Hlipala, Martin. "Futuristický kokpit moderního letounu." Master's thesis, Vysoké učení technické v Brně. Fakulta informačních technologií, 2020. http://www.nusl.cz/ntk/nusl-432956.

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This thesis is analysing the historical evolution of flight instruments and aims at the design of a new, enhanced cockpit that includes basic flight instruments supplemented by data from selected aircraft subsystems. The design is based on currently available electronic instruments, known as EFIS, presently used onboard Boeing 737-800 cockpit. The proposed design aims at improvements to graphic style of EFIS, and accomodation of new data into newly designed displays. As a result of this effort, a set of design concepts is created. Those are then implemented as fully functional set of displays

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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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40

Van, Wyk Robin. "Development of an integrated avionics hardware system for unmanned aerial vehicle research purposes." Thesis, Stellenbosch : University of Stellenbosch, 2011. http://hdl.handle.net/10019.1/6485.

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Thesis (MScEng (Electrical and Electronic Engineering))--University of Stellenbosch, 2011.<br>ENGLISH ABSTRACT: The development of an integrated avionics system containing all the required sensors and actuators for autopilot control is presented. The thesis analyzes the requirements for the system and presents detailed hardware design. The architecture of the system is based on an FPGA which is tasked with interfacing with the sensors and actuators. The FPGA abstracts a microprocessor from these interface modules, allowing it to focus only on the control and user interface algorithms. Fir

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41

Goodwin, Thomas David. "An implementation study of an accounting system design for the Naval Avionics Center." Thesis, Monterey, California. Naval Postgraduate School, 1991. http://hdl.handle.net/10945/28275.

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Sabatini, Roberto. "A novel avionics based GNSS integrity augmentation system for manned and unmanned aircraft." Thesis, University of Nottingham, 2017. http://eprints.nottingham.ac.uk/43912/.

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The aviation community has to implement very stringent navigation integrity requirements in a variety of manned and unmanned aircraft applications. This thesis presents the results of the research activities carried out by the Italian Air Force Research and Flight Test Centre (CSV-RSV) in collaboration with the Nottingham Geospatial Institute (NGI) and RMIT University in the area of Avionics Based Integrity Augmentation (ABIA) for mission-essential and safety-critical Global Navigation Satellite Systems (GNSS) applications in the civil/military aviation context. Space and Ground Based Augmenta

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43

Glas, Dylan F. (Dylan Fairchild) 1975. "Vehicle concept exploration and avionics architecture design for a fast package delivery system." Thesis, Massachusetts Institute of Technology, 2000. http://hdl.handle.net/1721.1/9253.

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Thesis (M.Eng.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2000.<br>Also available online at the MIT Theses Online homepage <http://thesis.mit.edu>.<br>Includes bibliographical references (leaves 96-97).<br>Fast Package Delivery was explored as a possible commercial application of advanced reusable launch vehicle technologies. The market was divided into two distinct segments: an on-demand charter service for urgent deliveries, and a scheduled service similar to today's overnight delivery services. System reliability is a strong driver for both cases. For th

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Perez, Alberto, John Hildin, and John Roach. "Design and Implementation of an Avionics Full Duplex Ethernet (A664) Data Acquisition System." International Foundation for Telemetering, 2008. http://hdl.handle.net/10150/606199.

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ITC/USA 2008 Conference Proceedings / The Forty-Fourth Annual International Telemetering Conference and Technical Exhibition / October 27-30, 2008 / Town and Country Resort & Convention Center, San Diego, California<br>ARINC 664 presents the designers of data acquisition systems challenges not previously seen on other aircraft avionic buses. Among the biggest challenges are providing the test instrumentation system with the capacity to process two redundant Ethernet segments that may be carrying packet traffic at near wire-line speed. To achieve this level of performance, the hardware and soft

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Dittrich, Joerg S. "Design and integration of an unmanned aerial vehicle navigation system." Thesis, Georgia Institute of Technology, 2002. http://hdl.handle.net/1853/15669.

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Sobron, Alejandro. "Design and Testing of a Flight Control System for Unstable Subscale Aircraft." Thesis, Linköpings universitet, Fluida och mekatroniska system, 2015. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-121819.

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The primary objective of this thesis was to study, implement, and test low-cost electronic flight control systems (FCS) in remotely piloted subscale research aircraft with relaxed static longitudinal stability. Even though this implementation was carried out in small, simplified test-bed aircraft, it was designed with the aim of being installed later in more complex demonstrator aircraft such as the Generic Future Fighter concept demonstrator project. The recent boom of the unmanned aircraft market has led to the appearance of numerous electronic FCS designed for small-scale vehicles and even

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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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Park, Sanghyuk 1973. "Avionics and control system development for mid-air rendezvous of two unmanned aerial vehicles." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/16662.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.<br>Includes bibliographical references (p. 177-181).<br>This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.<br>A flight control system was developed to achieve mid-air rendezvous of two unmanned aerial vehicles (UAVs) as a part of the Parent Child Unmanned Aerial Vehicle (PCUAV) project at MIT and the Draper Laboratory. A lateral guidance logic was developed for tightly tracking a desired flight path.

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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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