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Dissertations / Theses on the topic 'Flight simulator'

Author: Grafiati

Published: 4 June 2021

Last updated: 25 July 2025

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1

Bylander, Ulf. "Flight Path Simulation Application : A flight simulator for charged particle transport." Thesis, Uppsala universitet, Högenergifysik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-227759.

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CTF3 is a test facility for a new CLIC high energy linear collider. For this beamsteering and beam focusing is vital. Because physically running a beamline and changingsetup is expensive and takes much effort it is beneficial to use a simulator for thebeamline. The transportation of the beam through the beamline can be representedwith matrix multiplications and for this reason MATLAB is a fitting environment tosimulate in. A Flight Path Simulator was written in MATLAB and was succefullyimplemented and tested for the CALIFES beamline of the two-beam test stand that ispart of the CTF3 facility.

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2

Scamps, Alexander. "Development of a Variable Stability Flight Simulation Facility Re-engineering of Flight Control Loading and Motion Systems." Thesis, The University of Sydney, 2003. http://hdl.handle.net/2123/567.

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A Variable Stability Flight Simulator is being developed in the School of Aerospace, Mechanical and Mechatronic Engineering at the University of Sydney, Australia. The device is being developed both as a teaching tool for use in flight mechanics courses in the department and as a research tool. It is reasonable to state that learning is enhanced through the experience of concepts outside of the classroom environment. It is intended that the device will be integrated into the department�s teaching program in aircraft flight mechanics. Initial studies centred around a PC based flight simulat

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Scamps, Alexander. "Development of a Variable Stability Flight Simulation Facility Re-engineering of Flight Control Loading and Motion Systems." University of Sydney. Aerospace, Mechanical, 2003. http://hdl.handle.net/2123/567.

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A Variable Stability Flight Simulator is being developed in the School of Aerospace, Mechanical and Mechatronic Engineering at the University of Sydney, Australia. The device is being developed both as a teaching tool for use in flight mechanics courses in the department and as a research tool. It is reasonable to state that learning is enhanced through the experience of concepts outside of the classroom environment. It is intended that the device will be integrated into the department�s teaching program in aircraft flight mechanics. Initial studies centred around a PC based flight simulat

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4

Magnusson, Nählinder Staffan. "Flight Simulator Training : Assessing the Potential." Doctoral thesis, Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, 2009. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-17546.

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Mental workload is an important concept and has been proven to be a precursor to situation awareness and operative performance. This thesis describes methods to measure mental workload through self-ratings and psychophysiological measurements. Similarities and differences in psychophysiological reactions and rated mental workload between simulated and real flights are described. The consequences of such similarities and differences are discussed and its possible effect on training potential. A number of empirical studies are presented. They describe the experience and the psychophysiological r

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5

Kenney, Laurence P. J. "Flight simulator for special educational needs." Thesis, University of Salford, 1993. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.357202.

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6

Sikström, Tilda. "Flight Simulator Integration in Test Rig." Thesis, KTH, Flygdynamik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-299413.

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Integrating hardware in simulations is useful in many applications, for example to investigate the performance of an aircraft with the non-ideal response of a physical system. This thesis aims to integrate a flight simulator, JSBSim, with an actuator test rig, FLUMES Iron Bird. Two aircraft models were replicated in JSBSim, a passenger aircraft and a delta winged fighter aircraft. The models were analyzed to ensure proper flight performance in regards to stability. The stability analysis was conducted from both the aerodynamic data provided as well as through state-space theory. The fighter ai

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7

Helgesson, Fredrik. "Analysis of a flight mechanics simulator." Thesis, KTH, Flygdynamik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-265616.

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Aircraft design is an act of art requiring dedication and careful work to ensure good results. An essential tool in that work is a flight mechanics simulator. Such simulators are often built up of modules/models that are executed in a sequential order in each time iteration. This project aims to analyze potential improvements to the model execution order based on the dependency structure of one such simulator. The analysis method Design Structure Matrix (DSM), was used to define/map the dependencies and then Binary Linear Programming (BLP) was utilized to find five new potentially improved mod

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8

Elias, Joerg. "Advanced integrated helicopter flight simulator cockpit design." Thesis, Georgia Institute of Technology, 1989. http://hdl.handle.net/1853/12469.

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9

Johansson, Daniel. "Extending a battlefield simulator with large scale terrain rendering and flight simulator functionality." Thesis, Linköping University, Department of Science and Technology, 2005. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-5623.

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<p>Simulation of modern battlefield scenarios on consumer PC:s deal with a number of limitations, many of them related to the limited performance of a normal PC compared to workstations and servers. Specifically, the visualization of realistic large scale outdoor environments is problematic because of the large amount of data required to describe its contents. This becomes especially problematic in simulations of fast moving vehicles such as aircrafts, where one needs to maintain high frame rates while having high visual detail for orientation and targeting. This thesis proposes a method of ge

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10

Vazquez, Alan Andrew. "Touch screen use on flight simulator Instructor/Operator Stations." Thesis, Monterey, California : Naval Postgraduate School, 1990. http://handle.dtic.mil/100.2/ADA239524.

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Thesis (M.S. in Information Systems)--Naval Postgraduate School, September 1990.<br>Thesis Advisor(s): Lind, Judith H. ; Mitchell, Thomas. Second Reader: Haga, William J. "September 1990." Description based on title screen as viewed on December 18, 2009. Author(s) subject terms: Alternative Input, Touch Screen, Mouse, Trackball, Instructor/Operator Station, IOS, Data Entry Devices, Flight Simulators, User-Computer Interface. Includes bibliographical references (p. 70-71). Also available in print.

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11

Harvey, William. "Investigating the configuration of a flight training device for visual flight rules navigation." Thesis, Federation University Australia, 2020. http://researchonline.federation.edu.au/vital/access/HandleResolver/1959.17/174503.

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The acquisition of pilot navigational skills utilising visual landmarks is a crucial skill that is required as part of Visual Flight Rules navigation towards obtaining a Private Pilot License. Due to the high cost of pilot training simulators, industry has identified a need for research in efficient utilisation of low-end, low cost personal compute flight simulators to assist in developing pilot skills. Analysis of the effectiveness of the use of such personal computer simulators depend on proper configuration determined by measurable errors to define simulator fidelity. To date, research has

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12

Sagoo, Girish Kumar. "Pilot in loop assessment of fault tolerant flight control schemes in a motion flight simulator." Morgantown, W. Va. : [West Virginia University Libraries], 2008. https://eidr.wvu.edu/etd/documentdata.eTD?documentid=5800.

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Thesis (M.S.)--West Virginia University, 2008.<br>Title from document title page. Document formatted into pages; contains xiv, 121 p. : ill. (some col.), col. map. Includes abstract. Includes bibliographical references (p. 116-121).

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13

Root, Eric. "A Re-Configurable Hardware-in-the-Loop Flight Simulator." Ohio University / OhioLINK, 2004. http://www.ohiolink.edu/etd/view.cgi?ohiou1090939388.

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14

O'Neill, Jennifer K. "Backdriving a full motion simulator using flight recorder data." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape3/PQDD_0015/MQ53325.pdf.

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15

Benet, C., M. Wickham, and J. Balzer. "THE COMSAT ATTITUDE AND ORBIT CONTROL SYSTEM FLIGHT SIMULATOR." International Foundation for Telemetering, 1986. http://hdl.handle.net/10150/615296.

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International Telemetering Conference Proceedings / October 13-16, 1986 / Riviera Hotel, Las Vegas, Nevada<br>The success of a communications satellite mission depends not only on the proper operation of the on-board Attitude and Orbit Control System (AOCS), but also on the complex interaction between the spacecraft and the ground control center. In support of a satellite program from its inception to launch and throughout the inorbit life, COMSAT has developed a SATELLITE ATTITUDE AND ORBIT CONTROL SYSTEM FLIGHT SIMULATOR. This paper describes the design and operations of the COMSAT FLIGHT

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Rogerson, Stuart Peter. "Implementation of a distributed interactive simulation interface in a Sea King flight simulator." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp04/mq29371.pdf.

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17

Dennis, K. A. "An evaluation of the utility of a Personal Computer-based Aviation Training Device (PCATD) for private pilot's licence training." Thesis, Cranfield University, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.267495.

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18

Le-Ngoc, Luan. "Augmenting low-fidelity flight simulation training devices via amplified head rotations." Thesis, Loughborough University, 2013. https://dspace.lboro.ac.uk/2134/14441.

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Due to economic and operational constraints, there is an increasing demand from aviation operators and training manufacturers to extract maximum training usage from the lower fidelity suite of flight simulators. It is possible to augment low-fidelity flight simulators to achieve equivalent performance compared to high-fidelity setups but at reduced cost and greater mobility. In particular for visual manoeuvres, the virtual reality technique of head-tracking amplification for virtual view control enables full field-of-regard access even with limited field-of-view displays. This research quantif

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19

Sherman, Kim L. "The design and construction of a hang glider flight simulator /." Online version of thesis, 1992. http://hdl.handle.net/1850/11260.

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20

Donati, Dario. "Analysis of aircraft load spectrum by means of flight simulator." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2015. http://amslaurea.unibo.it/9346/.

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Damage tolerance analysis is a quite new methodology based on prescribed inspections. The load spectra used to derive results of these analysis strongly influence the final defined inspections programs that for this reason must be as much as possible representative of load acting on the considered structural component and at the same time, obtained reducing both cost and time. The principal purpose of our work is in improving the actual condition developing a complete numerical Damage Tolerance analysis, able to prescribe inspection programs on typical aircraft critical components, respecting

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21

Misovec, Kathleen. "The effect of flight simulator motion on modelled vestibular response." Thesis, Massachusetts Institute of Technology, 1986. http://hdl.handle.net/1721.1/83660.

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Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1986.<br>Microfiche copy available in Archives and Barker.<br>Bibliography: leaves [133]-[134].<br>by Kathleen M. Misovec.<br>M.S.

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22

Joensen, Daniel Eide. "Let's Go--Home Depot : development of a management flight simulator." Thesis, Massachusetts Institute of Technology, 1993. http://hdl.handle.net/1721.1/12382.

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23

Olsson, Tobias, and Oscar Ullberg. "Mixed Reality for Gripen Flight Simulators." Thesis, Linköpings universitet, Medie- och Informationsteknik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-173831.

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This thesis aims to evaluate how different mixed reality solutions can be built and whetheror not it could be used for flight simulators. A simulator prototype was implemented usingUnreal Engine 4 with Varjo’s Unreal Engine plugin giving the foundation for the evaluations done through user studies. Three user studies were performed to test subjectivelatency with Varjo XR-1 in a mixed reality environment, test hand-eye coordination withVarjo XR-1 in a video see-through environment, and test the sense of immersion betweenan IR depth sensor and chroma key flight simulator prototype. The evaluatio

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Fujizawa, Brian T. "Control Law Design and Validation for a Helicopter In-Flight Simulator." DigitalCommons@CalPoly, 2010. https://digitalcommons.calpoly.edu/theses/240.

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In-flight simulation allows one aircraft to simulate the dynamic response of another aircraft. A control system designed to give RASCAL, a JUH-60A Black Hawk helicopter based at Moffett Field, CA, in-flight simulation capabilities has been designed, optimized and validated in this research. A classical explicit model following control system with a frequency dependent feedback controller was used. The frequency dependent controller allows model following of the attitude in the short term and the velocity in the long term. Controller gains were optimized using a high order, linearized model

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25

Pradipta, Justin [Verfasser]. "Development of a Pneumatically Driven Flight Simulator Motion Platform / Justin Pradipta." Aachen : Shaker, 2016. http://d-nb.info/1138177989/34.

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26

Beluzo, Carlos Eduardo. "Programa computacional para um simulador de vôo." Universidade de São Paulo, 2006. http://www.teses.usp.br/teses/disponiveis/18/18135/tde-08012016-114920/.

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Os simuladores de vôo têm sido uma importante ferramenta para treinamento de pilotos e análise de vôo sem ter que se desembolsar grandes quantias monetárias, economizando combustível e evitando acidentes. Conseqüentemente, a demanda por simuladores de vôo tem aumentado tanto na indústria quanto na pesquisa. Com o intuito de futuramente construir um simulador de vôo, foi desenvolvido um projeto para elaboração de um software capaz de simular uma aeronave em vôo, do ponto de vista de dinâmica de vôo. O software SIMAERO foi desenvolvido na linguagem de programação C++ e simula a dinâmica de vôo d

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27

Jurta, Daniel S. "Validation of the USNTPS simulator for the advanced flight controls design exercise." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Dec%5FJurta.pdf.

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28

Lawn, Peter. "The enhancement of a flight simulator system with teaching and research applications." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1998. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp01/MQ39982.pdf.

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29

McKavitt, Thomas Patrick Jr. "Parameter identification studies on the NASAAMES Research Center Advanced Concepts Flight Simulator." Thesis, Monterey, California: Naval Postgraduate School, 1990. http://hdl.handle.net/10945/34911.

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Approved for public release; distribution unlimited.<br>The results of an aircraft parameters identification study conducted on the National Aeronautics and Space AdministrationAmes Research Center Advanced Concepts Flight Simulator (ACFS) in conjunction with the Navy-NASA joint Institute of Aeronautics are given. The ACFS is a commercial airline simulator with a design based on future technology. The simulator is used as a laboratory for human factors research and engineering as applied to the commercial airline industry. Parametric areas examined were engine pressure ratio (EPR), optimum lon

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Palmqvist, Tor. "Night Vision in an Unreal Engine 4-Based Virtual Reality Flight Simulator." Thesis, Linköpings universitet, Institutionen för datavetenskap, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-166650.

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Att utnyttja simuleringsteknologi är både ett effektivt och sparsamt sätt att träna piloter utan att utsätta sig själv eller andra för fara. Flygsimuleringar i Virtual Reality blir mer och mer eftersökta tack vare sin unika nivå av immersion. Detta arbete undersöker, utvärderar och visar hur night vision implementeras i Unreal Engine 4. Undersökningen kommer fram till sex specificerade nyckelfaktorer att följa för att korrekt kunna simulera night vision och visar hur detta uppnås huvudsakligen genom att konfigurera post process-effekter. Dessutom utvärderas implementationens prestanda baserat

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31

Bauer, Maria. "EVALUATING THE EFFECTIVENESS OF TRAINING SYSTEM APPROACHES FOR HIGHLY COMPLEX FLIGHT TRAINING." Doctoral diss., University of Central Florida, 2005. http://digital.library.ucf.edu/cdm/ref/collection/ETD/id/3020.

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This research investigates the Training Effectiveness of a low-cost, PC-based training system when compared with two modes (motion and no motion) of a cab training system with large screen for various aviation flying tasks. While much research on this topic has been done in the past, advances in technology have significantly altered what is considered a "low-cost" "simulator." The technology advances have in effect increased the ability of a "low-cost" "simulator" to deliver desired experiences to the user. These "simulators" often are nothing more than PC training system, with only notional r

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Persson, Daniel. "Passenger Flight Experience of Urban Air Mobility." Thesis, Uppsala universitet, Observationell astrofysik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-399699.

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The first part of a study of passenger flight experience of Urban Air Mobility was completed. This first part included the design of different Urban Air Mobility vehicle models, in which the passenger flight experience would be quantitatively measured. A first version of a simulator setup, in which the measurements were performed, was also developed. Three concept vehicle models, a single main rotor, a side-by-side rotor and a quadrotor, were designed in the conceptual design software NDARC. The vehicles were electrically propelled with battery technology based on future technology predictions

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Senneberg, Sofia. "Methods for validating a flight mechanical simulation model for dynamic maneuvering." Thesis, KTH, Flygdynamik, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-299412.

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Flight mechanical simulators play an important role in the design steps during development of a new aircraft. To be able to simulate and evaluate flight mechanical characteristics during development it is important to minimize development time and cost while keeping flight safety high during early flights. The aim of the project presented in this thesis is to develop a method for validating a flight mechanical simulator against flight test data from dynamic maneuvering. An important part in this thesis is about how deviations in the result data can be found and analyzed, for example deviations

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34

Hernandez, Luis. "Causality tracing user interface design and development for a software management flight simulator." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1995. http://handle.dtic.mil/100.2/ADA305650.

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Thesis (M.S. in Information Technology Management) Naval Postgraduate School, December 1995.<br>Thesis advisor(s): T. Hamid, B. Ramesh. "December 1995." Bibliography: p. 177-178. Also available online.

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35

MacInnis, Daniel V. 1964. "Development of a system dynamics based management flight simulator for new product development." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/34732.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design & Management Program, 2004.<br>Includes bibliographical references (p. 152-153).<br>All firms in any mature product development industry are being pressured into performing 'better, faster, and cheaper' by both customers and competitors. In short, firms are being tasked with doing more, with less, faster. This leads to product development organizations being unrealistically tasked to deliver on these programs that often lead to projects falling behind schedule, over budget, and with inadequate quality. While striving to do the

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36

McKavitt, Thomas P. "Parameter identification studies on the NASA/AMES Research Center Advanced Concepts Flight Simulator." Monterey, California : Naval Postgraduate School, 1990. http://handle.dtic.mil/100.2/ADA240587.

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Thesis (M.S. in Aeronautical and Astronautical Engineer)--Naval Postgraduate School, September 1990.<br>Thesis Advisor(s): Schmidt, Louis V. Second Reader: Howard, Richard M. "September 1990." Description based on title screen as viewed on March 19, 2010. DTIC Identifier(s): Parameter Identification, Aircraft Simulator. Author(s) subject terms: Parameter Identification, Aircraft Simulator, Advanced Concepts Flight Simulator, ACFS. Includes bibliographical references (p. 57). Also available in print.

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37

Lindqvist, Daniel. "Methodology For Evaluating Flying Qualities From Desktop Simulator." Thesis, Luleå tekniska universitet, Rymdteknik, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-77354.

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A modern ghter aircraft has an advanced ight control system which highly augmentsthe control inputs from the pilot. To verify a new iteration of the control system is a timeconsuming and expensive task. It is desired to nd qualities that is not satisfactory to thepilot as early as possible in the verication process to reduce the cost for design changes.The primary objective of this thesis is to develop methods that can be used for automaticalevaluation of aircraft ying qualities from the data provided by a desktop simulator. A desktopsimulator is cheap to use compared to ight tests and tests w

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Rekleitis, Georgios. "Modeling and evaluation of a new parallel mechanism as a flight simulator motion base." Thesis, McGill University, 2003. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=80137.

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In this thesis, a novel 6 degree-of-freedom parallel mechanism is evaluated as a flight simulator motion base. The mechanism consists of three fixed-length legs, each supported by a three-wheeled mobile robot. The three legs support a platform, which acts as the end-effector of the mechanism. Thus, the mechanism has the advantage of portability and simple design, because of the specific actuating system. Two different designs are evaluated: one with ball joints at the upper ends of the legs and revolute joints at the lower ends and one with the opposite configuration. The inverse kinema

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Sullivan, Robert Bryan. "The use of vestibular models in flight simulator motion washout systems : an experimental evaluation." Thesis, Massachusetts Institute of Technology, 1985. http://hdl.handle.net/1721.1/80443.

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Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1985.<br>Microfiche copy available in Archives and Barker.<br>Bibliography: leaves 114-115.<br>by Robert Bryan Sullivan.<br>M.S.

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Grogan, Andrew S. "A Low Cost, Portable Stewart Platform Study for Flight Simulation and Gaming Simulation." Ohio University / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1606121360298874.

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McNamara, William G., Page Stanley, and Jay Nichols. "RTPS Telemetry - Simulator Link at Naval Air Warfare Center." International Foundation for Telemetering, 1995. http://hdl.handle.net/10150/611514.

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International Telemetering Conference Proceedings / October 30-November 02, 1995 / Riviera Hotel, Las Vegas, Nevada<br>Over the last 3 years the Naval Air Warfare Center Aircraft Division (NAWCAD), Patuxent River, MD, has been in the process of developing a link between its secure Manned Flight Simulator (MFS) and Real Time Processing System (RTPS) facilities. The MFS hosts a wide variety of high fidelity fixed and rotary wing aircraft simulation models. The RTPS is used as a telemetry ground station for conduct of Navy flight testing at Patuxent River MD. The ability to integrate simulation w

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McMullen, Eric L., and Brian Shane Grass. "EFFECTS OF UAV SUPERVISORY CONTROL ON F-18 FORMATION FLIGHT PERFORMANCE IN A SIMULATOR ENVIRONMENT." Monterey, California. Naval Postgraduate School, 2013. http://hdl.handle.net/10945/32870.

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Continual advances in technology, along with increased cockpit workload particularly the shift from two-seat to single-seat fighters to save money and reduce risk to lifepush the limits of human mental capacity. Additionally, there is interest within the military aviation community to integrate Unmanned Aerial Vehicle (UAV) control into the cockpit in order to expand force projection capability. This study compared the effects on formation flight performance of two different secondary tasks, specifically a traditional secondary task such as target prosecution with an electro-optical Forward Lo

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Söderström, Arvid, and Johanna Thorheim. "Design and evaluation of an educational tool for understanding functionality in flight simulators : Visualising ARINC 610C." Thesis, Linköpings universitet, Interaktiva och kognitiva system, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-137686.

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The use of simulation in aircraft development and pilot training is essential as it saves time and money. The ARINC 610C standard describes simulator functionality, and is developed to streamline the use of flight simulators. However, the text based standard lacks overview and function descriptions are hard to understand for the simulator developers, who are the main users. In this report, an educational software tool is conceptualised to increase usability of ARINC 610C. The usability goals and requirements were established through multiple interviews and two observation studies. Consequently

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Davis, Richard D. "Design and development of a user interface and user manual for the Software Management Flight Simulator." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1995. http://handle.dtic.mil/100.2/ADA303352.

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Thesis (M.S. in Information Technology Management) Naval Postgraduate School, September 1995.<br>Thesis advisor(s): T. Hamid, H.K. Bhargava. "September 1995." Includes bibliographical references. Also available online.

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Cetin, Yasemin. "Evaluation Of Visual Cues Of Three Dimensional Virtual Environments For Helicopter Simulators." Master's thesis, METU, 2008. http://etd.lib.metu.edu.tr/upload/2/12610100/index.pdf.

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Flight simulators are widely used by the military, civil and commercial aviation. Visual cues are an essential part of helicopter flight. The required cues for hover are especially large due to closeness to the ground and small movements. In this thesis, density and height parameters of the 3D (Three Dimensional) objects in the scene are analyzed to find their effect on hovering and low altitude flight. An experiment is conducted using a PC-based flight simulator with three LCD monitors and flight control set. Ten professional military pilots participated in the experiment. v Results revealed

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Diab, Hassan Bahaeddine. "Microprocessor based real-time modelling in relation to the visual systems of an aircraft flight-training simulator." Thesis, University of Bath, 1985. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.353694.

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The purpose of this thesis is to show the application of modern digital techniques to produce a high speed computational system that has the capability of producing a faster than real-time model for the visual systems associated with flight simulator systems. A distributed/multiprocessing system was chosen due to the increased reliability, flexibility and throughput of the computational process. The system also has the advantage of providing increased modularity and ease of expansion. This research is firstly concerned with the development of a high resolution graphics system (providing a 1024

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Friedenthal, Stephen R. (Stephen Roger). "Developing a risk management "flight simulator" for manned space programs : a user interface to a system dynamic simulation of system safety at NASA." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/34630.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design and Management Program, February 2006.<br>Includes bibliographical references (p. 81-82).<br>Simulators are a staple of any engineering project and manned space flight in particular. From pilot and crew training to maintenance and emergency repairs, very little is done without it first being thoroughly practiced and refined during advance simulation. Whether the simulation uses a computerized flight simulator that recreates the physics and experience of flight, or a simple mock-up with paper cutouts and hand tools, the end res

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Casto, Kristen Lee. "An Examination of Headset, Hearing Sensitivity, Flight Workload, and Communication Signal Quality on Black Hawk Helicopter Simulator Pilot Performance." Diss., Virginia Tech, 2009. http://hdl.handle.net/10919/28664.

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Among the many occupational hazards to which Army rotary-wing aviators are exposed is intense noise generated from the aircraft. The potential for permanent hearing loss and difficulty communicating in helicopter noise is well known; an appropriate way to evaluate a hearing-impaired pilotâ s safety risk due to hearing loss is not as well known. Previous research has studied communication ability in helicopter cockpit noise under different headsets, but there are not conclusive data on the combined effects of degraded speech intelligibility due to noise and flight workload under the headset

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Eliasson, Carl, and Alexander Hedberg. "VR-flygsimulatorer, för ökad upplevelse och som läroverktyg i flygutbildningar." Thesis, Mälardalens högskola, Akademin för innovation, design och teknik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:mdh:diva-35667.

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Virtual reality (VR) är ett begrepp som blivit allt mer välkänt de senaste åren. VR kan beskrivas som en datorgenererad virtuell omvärld som användaren omsluts av. VR-miljön upplevs genom människans sinnen såsom syn, hörsel och känsel.Syftet med examensarbetet är att undersöka hur realistisk en kommersiellt tillgänglig VR-flygsimulator upplevs av piloter och undersöka om VR-teknik kan vara ett användbart läroverktyg för t.ex. flygskolor. VR-tekniken har under de senaste åren utvecklats väldigt mycket vilket gjort att många av de implementations svårigheter som VR-tekniken inneburit till stor d

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Nikolic, Mark I. "The human-machine teams create, explain, and recover from coordination breakdowns: a simulator study of disturbance management on modern flight decks." The Ohio State University, 2004. http://rave.ohiolink.edu/etdc/view?acc_num=osu1092808745.

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