Relevant bibliographies by topics / Aircraft cockpits

Contents

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

Academic literature on the topic 'Aircraft cockpits'

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

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Journal articles on the topic "Aircraft cockpits"

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Lindo, Roneil S., John E. Deaton, John H. Cain, and Celine Lang. "Methods of Instrument Training and Effects on Pilots’ Performance With Different Types of Flight Instrument Displays." Aviation Psychology and Applied Human Factors 2, no. 2 (January 2012): 62–71. http://dx.doi.org/10.1027/2192-0923/a000028.

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As computer display technology has evolved, so have the aircraft instrument displays pilots use for aircraft control and navigation. With the aid of two different flight training devices – one configured with steam gauges and the other configured with glass cockpit – this study measured aircraft control and navigation differences between two pilot groups. Pilot Group 1 had earned their instrument rating in aircraft equipped with steam gauges, and Pilot Group 2 had earned their instrument rating in aircraft equipped with glass cockpits. Using displays for which they were not trained, each pilot was tested on aircraft control and navigation precision. The test required that pilots complete basic instrument maneuvers and an instrument landing system approach. Using MANOVA, deviations from assigned values were recorded and statistically compared. Study findings indicated that steam gauge pilots transitioning to glass cockpits perform better than glass cockpit pilots transitioning to steam gauge displays.
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Hettinger, Lawrence J., W. Todd Nelson, and Michael W. Haas. "Applying Virtual Environment Technology to the Design of Fighter Aircraft Cockpits: Pilot Performance and Situation Awareness in a Simulated Air Combat Task." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 38, no. 1 (October 1994): 115–18. http://dx.doi.org/10.1177/154193129403800123.

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The use of multi-sensory displays for fighter aircraft cockpits is being investigated at the U.S. Air Force's Armstrong Laboratory as a means of enhancing pilot performance. The current experiment was conducted to evaluate the effect of employing such displays on the performance of a simulated air combat task. Each of four experienced US Air Force F-16 pilots flew 12 simulated missions which required them to locate and destroy four enemy bombers whose flight path was pre-programmed. Simultaneously, two other pilots were assigned to auxiliary cockpits in the laboratory and flew enemy fighter aircraft in an attempt to intercept and shoot down the primary pilot. Therefore there were three active participants in each air combat scenario. Each pilot flew six trials using a cockpit comprised of conventional F-15 flight instruments and six trials using a modified, multi-sensory cockpit. The results indicated that pilot performance and situation awareness were generally superior with the multi-sensory cockpit as opposed to the conventional cockpit, although statistical differences between the two were at best marginally significant. Nevertheless, the results suggest that if pilots were to receive advance training with the multi-sensory cockpit their performance may exceed that in the highly overlearned conventional cockpit by even more substantial amounts.
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Endsley, Mica R. "Design and Evaluation for Situation Awareness Enhancement." Proceedings of the Human Factors Society Annual Meeting 32, no. 2 (October 1988): 97–101. http://dx.doi.org/10.1177/154193128803200221.

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Situation awareness (SA) is an important component of pilot/system performance in all types of aircraft. It is the role of the human factors engineer to develop aircraft cockpits which will enhance SA. Research in the area of situation awareness is is vitally needed if system designers are to meet the challenge of providing cockpits which enhance SA. This paper presents a discussion of the SA construct, important considerations facing designers of aircraft systems, and current research in the area of SA measurement.
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Kolbeinsson, Ari, Göran Falkman, and Jessica Lindblom. "Showing Uncertainty in Aircraft Cockpits using Icons." Procedia Manufacturing 3 (2015): 2905–12. http://dx.doi.org/10.1016/j.promfg.2015.07.805.

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Voge, Victoria, and Lance Schaeffer. "POTENTIAL RAINBOE TOXICITY IN COMMERCIAL AIRCRAFT COCKPITS." Southern Medical Journal 89, Supplement (October 1996): S70. http://dx.doi.org/10.1097/00007611-199610001-00133.

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Liu, Xin, Sui Huai Yu, Tian Cheng Gong, Qing Zhang, Ming Lei Zhao, and Wan Yu Zhang. "Ergonomics Layout Optimization of the Aircraft Cockpit Based on Particle Swarm Optimization." Advanced Materials Research 1044-1045 (October 2014): 1851–54. http://dx.doi.org/10.4028/www.scientific.net/amr.1044-1045.1851.

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The problem of neglecting ergonomic factors on the aircraft cockpit layout design which leads to the pilots feeling tired very soon should be solved imminently. Since there are a lot of ergonomic constraints while there are hardly any algorithms to solve the problem, the particle swarm optimization is mentioned. Firstly, ergonomic geometric constraints and ergonomic space constraints are confirmed. Secondly, the objective function is confirmed based on the minimum Euclidean distance. Thirdly, to avoid local optimum, particle swarm optimization is used to find the best coordinate values of facilities. At last, the best values of different facilities are needed to be compromised by each other to confirm the most proper values for every facility and form the optimal scheme of designing the layout of aircraft cockpits.
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Way, Thomas C. "3-D in Pictorial Formats for Aircraft Cockpits." Proceedings of the Human Factors Society Annual Meeting 33, no. 2 (October 1989): 23–27. http://dx.doi.org/10.1177/154193128903300205.

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Sixteen military pilots flew simulated air-to-air and air-to-ground missions in a simulated fighter-attack cockpit. Three of the five color CRTs in the cockpit were capable of displaying retinal disparity and the major independent variable was presence or absence of disparity. Performance, workload, and opinion data were collected. A second objective of the study was to continue development of the display formats, which had evolved through earlier projects. The disparity results and the recommended format revisions are presented.
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Gregoire, Harv, and Rannell Dahl. "Anthropometric Design Criteria: Correction Variables for Military Aircraft." Perceptual and Motor Skills 68, no. 1 (February 1989): 175–78. http://dx.doi.org/10.2466/pms.1989.68.1.175.

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Significant errors in the application of dimensional anthropometric design criteria for tactical military aircraft cockpits have been identified. These errors result from insufficient consideration of previously undefined variables relative to posture, restraint system items, and aviators' personal protection equipment as discussed by McConville and Laubach in 1978.
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Segal, Leon D. "Actions Speak Louder than Words: How Pilots use Nonverbal Information for Crew Communications." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 38, no. 1 (October 1994): 21–40. http://dx.doi.org/10.1177/154193129403800106.

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How does the design of an aircraft cockpit affect crew communication? The research described hereunder aimed at identifying aspects of design that play a critical role in task coordination, yet have heretofore been ignored. It is proposed that crewmembers coordinate the performance of tasks using visual, nonverbal, information that emerges from the interactions between individual pilots and the aircraft's systems. 24 airline pilots participated in a high-fidelity simulator experiment which compared the impact of three different types of interface on crew communication and coordination. Measurement included detailed video recording, and quantitative and expert performance evaluations. The data suggest that pilots visually monitor each other's performance of tasks, that visual monitoring is affected by the design of the interface, and that pilots rely on such nonverbal information for communication and coordination. The discussion looks at implications of these data to the design of workstations and cockpits.
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Gratton, G. B. "Use of Global Positioning System velocity outputs for determining airspeed measurement error." Aeronautical Journal 111, no. 1120 (June 2007): 381–88. http://dx.doi.org/10.1017/s0001924000004632.

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Abstract Several methods have been derived since the advent of GPS (Global Positioning System) receivers in aircraft cockpits by which these receivers may be used to calibrate these aircraft’s other instrumentation; in particular the pitot-static system. This paper presents the four most suitable methods, two of which have been developed by the author. These methods are shown with a common symbology, and their strengths, weaknesses, analysis and operational use are compared.
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Dissertations / Theses on the topic "Aircraft cockpits"

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Zehner, Gregory F. "Prediction of anthropometric accommodation in aircraft cockpits /." The Ohio State University, 2000. http://rave.ohiolink.edu/etdc/view?acc_num=osu1488203857251563.

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Bador, Damien (Damien Pierre Marcellin Dominique). "Improving commonality implementation in the cockpits of commercial aircraft." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/40895.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (S.M.)--Massachusetts Institute of Technology, Engineering Systems Division, 2007.
Includes bibliographical references (p. 143-154).
Product development is a major source of competitive advantage in the commercial aircraft business. Judiciously implementing commonality across a range of products yields important benefits in this area. Thus, measuring the quality of commonality implementation is extremely beneficial for aircraft manufacturers. This thesis analyses the concept of commonality and divides it into three constructs that can help understand all of its aspects: standardization, reusability and modularity. This work then presents a set of metrics measuring each of these aspects, from the point of view of the manufacturer and of the customer. The appropriateness of this set of metrics is then tested in a case study analyzing the efficiency of commonality implementation in the cockpit of two well-known commercial aircraft families: the Airbus A320 family and the Boeing 737 family. This thesis further describes what additional analysis should be performed to validate the set of metrics for broader applications. After documenting the efficiency of the set of metrics, this thesis analyses the current practices of commonality management in commercial aviation. It finally explores some of the limitations of the concept of commonality and sketches solutions to overcome them.
by Damien Bador.
S.M.
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New, Michael Dean. "Deactivation of automation in aircraft systems using dynamic function allocation." Thesis, Georgia Institute of Technology, 1996. http://hdl.handle.net/1853/28792.

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Kolbeinsson, Ari. "Visualising uncertainty in aircraft cockpits : Is icon degradation an appropriate visualisation form." Thesis, Högskolan i Skövde, Institutionen för kommunikation och information, 2013. http://urn.kb.se/resolve?urn=urn:nbn:se:his:diva-8342.

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Visualising uncertainty information has been a research area for the past decade or so, and this thesis contains the results of an experiment that examines whether prior research on icon degradation for showing uncertainty can be used in a simulated aircraft cockpit environment. Using icon degradation has been suggested as being effective to combat overconfidence bias, as well as to accurately convey information about uncertainty. Two icon sets using icon degradation were taken from prior research, and one new icon set using shape change and colour change was created for comparison. Subjects flew a flight simulator while reading icons to evaluate the uncertainty displayed, and also evaluating their own confidence in their reading. The results show that shape change leads to much higher accuracy in reading icons, and slightly higher levels of confidence. Furthermore, icon degradation results in a higher variance in reading icons and an increase in errors when no time-pressure or distraction is present. This suggests that the suitability of icon degradation for showing uncertainty is questionable in all situations, and that other design approaches such as shape change should be considered. Furthermore, problems were uncovered in the prior research that the old icons were taken from, and these problems call into question the general approach used in that research. Keywords: Uncertainty visualisation, Naturalistic decision-making, NDM, Aviation, Aircraft cockpit, Decision support, Situation assessment, Threat assessment.
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Chen, Ted L. "Design and evaluation of an in-cockpit re-planning tool as an emergency decision aid." Thesis, Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/12240.

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Fayollas, Camille. "Architecture logicielle générique et approche à base de modèles pour la sûreté de fonctionnement des systèmes interactifs critiques." Thesis, Toulouse 3, 2015. http://www.theses.fr/2015TOU30114/document.

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Depuis l'introduction au début des années 2000 du standard ARINC 661 (définissant les interfaces graphiques dans les cockpits), les avions modernes, tels que l'A380, l'A350 ou le B787, intègrent des systèmes interactifs permettant à l'équipage d'interagir avec des applications interactives. Ces applications sont affichées sur des écrans à travers l'utilisation d'un dispositif similaire à un clavier et une souris. Pour des raisons d'exigences de sûreté de fonctionnement, l'utilisation de ces systèmes est limitée, à l'heure actuelle, à la commande et au contrôle de fonctions avioniques non critiques. Cependant, l'utilisation de ces systèmes dans les cockpits d'avions civils apporte de nombreux avantages (tels qu'une amélioration de l'évolutivité du cockpit) qui amènent les industriels à chercher comment l'étendre à la commande et le contrôle de systèmes avioniques critiques. Dans cette optique, nous proposons une approche duale et homogène de prévention et de tolérance aux fautes pour concevoir et développer des systèmes interactifs tolérants aux fautes. Celle-ci repose, dans un premier temps, sur une approche à base de modèles permettant de décrire de manière complète et non ambiguë les composants logiciels des systèmes interactifs et de prévenir les fautes logicielles de développement. Dans un second temps, elle repose sur une approche de tolérance aux fautes naturelles et certaines fautes logicielles résiduelles en opération, grâce à la mise en œuvre d'une solution architecturale fondée sur le principe des composants autotestables. Les contributions de la thèse sont illustrées sur une étude de cas de taille industrielle : une application interactive inspirée du système de commande et contrôle de l'autopilote de l'A380
Since the introduction of the ARINC 661 standard (that defines graphical interfaces in the cockpits) in the early 2000, modern aircrafts such as the A380, the A350 or the B787 possess interactive systems. The crew interacts, through physical devices similar to keyboard and mouse, with interactive applications displayed on screens. For dependability reasons, only non-critical avionics systems are managed using such interactive systems. However, their use brings several advantages (such as a better upgradability), leading aircraft manufacturers to generalize the use of such interactive systems to the management of critical avionics functions. To reach this goal, we propose a dual and homogeneous fault prevention and fault tolerance approach. Firstly, we propose a model-based approach to describe in a complete and unambiguous way interactive software components to prevent as much as possible development software faults. Secondly, we propose a fault tolerant approach to deal with operational natural faults and some residual software faults. This is achieved through the implementation of a fault tolerant architecture based on the principle of self-checking components. Our approach is illustrated on a real size case study: an interactive application based on the command and control system of the A380 autopilot
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Carmody, Meghan A. "Task-Dependent Effects of Automation: The Role of Internal Models in Performance, Workload, and Situational Awareness in a Semi-Automated Cockpit." Ft. Belvoir Defense Technical Information Center, 1994. http://handle.dtic.mil/100.2/ADA292538.

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Schoberg, Paul R. "Secure ground-based remote recording and archiving of aircraft "Black Box" data." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03sep%5FSchoberg.pdf.

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Thesis (M.S. in Computer Science)--Naval Postgraduate School, September 2003.
Thesis advisor(s): Cynthia E. Irvine, Scott Cote. Includes bibliographical references (p. 169-171). Also available online.
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Altug, Muhittin Nami. "Structural Analysis Of A Jet Trainer Cockpit." Master's thesis, METU, 2012. http://etd.lib.metu.edu.tr/upload/12614086/index.pdf.

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This thesis presents structural analysis of a cockpit of a jet trainer type aircraft and the correlation studies performed by using ground pressurisation test results. For this purpose, first the response of the complex integrated fuselage structure is investigated under the complex type cabin pressure load. Then, cockpit part of the fuselage structure is modelled using commercial finite element software MSC/PATRAN®
and MSC/NASTRAN®
. The finite element model (FEM) of the cockpit structure is improved by the examination of the ground pressurisation test data and is finalised after achieving a good correlation between the finite element analysis (FEA) and the test results. This final form of the FEM of the cockpit structure serving as a benchmark is proved to be reliable for any future modifications.
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Rohre, Stuart M. "QUALIFYING THE COCKPIT VOICE RECORDER AS AN INSTRUMENTATION RECORDER AND AIRCRAFT STRUCTURAL MONITORING INSTRUMENT." International Foundation for Telemetering, 1998. http://hdl.handle.net/10150/607385.

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International Telemetering Conference Proceedings / October 26-29, 1998 / Town & Country Resort Hotel and Convention Center, San Diego, California
A novel concept using the cockpit voice recorder (CVR) as a structural vibration recording device, to aid in structural health monitoring of commercial and military aircraft, is outlined. The unused cables in the CVR wiring harness act as “latent transducers” that respond to structural vibrations, generating vibration signals, which the CVR records. Postprocessing of such data can provide clues to problem areas or changes in the signature of the aircraft. The standards which the CVR must meet to qualify as a instrumentation-quality recorder are discussed and the steps required to assure compliance are outlined.
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Books on the topic "Aircraft cockpits"

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Fighting cockpits, 1914-2000: Design and development of military aircraft cockpits. Shrewsbury, England: Airlife, 1999.

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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Visual effects in the high performance aircraft cockpit. Neuilly sur Seine, France: AGARD, 1988.

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Control in the sky: The evolution and history of the aircraft cockpit. Barnsley: Pen & Sword Aviation, 2005.

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Germany) International Workshop on Aircraft System Technologies (4th 2013 Hamburg. Proceedings of the 4th International Workshop on Aircraft System Technologies: April 23-24, 2013, Hamburg, Germany. Aachen: Shaker, 2013.

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Lutat, Christopher J. Automation airmanship: Nine principles for operating glass cockpit aircraft. New York: McGraw-Hill Education, 2013.

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Mikesh, Robert C. Japanese aircraft interiors, 1940-1945. Sturbridge, MA: Monogram Aviation Pub., 2000.

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Canada. Department of National Defence. Canadian Engineering Centennial Convention papers. Ottawa: National Defence Headquarters, 1987.

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Miller, Stephen P. Detecting mode confusion through formal modeling and analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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Miller, Stephen P. Detecting mode confusion through formal modeling and analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Advanced aircraft interfaces: the machine side of the man-machine interface: Papers presented at the Avionics Panel Symposium held in Madrid, Spain, 18th-22nd May 1992. Neuilly sur Seine, France: AGARD, 1992.

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Book chapters on the topic "Aircraft cockpits"

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Wilkinson, Peter R. "The Qualification of Military Aircraft Cockpits." In Verification and Validation of Complex Systems: Human Factors Issues, 593–608. Berlin, Heidelberg: Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-662-02933-6_43.

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Ohlander, Ulrika, Jens Alfredson, Maria Riveiro, and Göran Falkman. "Informing the Design of Fighter Aircraft Cockpits Using a Teamwork Perspective." In Advances in Intelligent Systems and Computing, 3–10. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-93885-1_1.

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Foudhaili, Hatem, and Eduard Reithmeier. "Concepts of Active Noise Aircraft Cockpits Reduction Employed in High Noise Level." In Variational Analysis and Aerospace Engineering, 229–41. New York, NY: Springer New York, 2009. http://dx.doi.org/10.1007/978-0-387-95857-6_13.

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Barbé, Jérôme, Marion Wolff, and Régis Mollard. "Human Centered Design Approach to Integrate Touch Screen in Future Aircraft Cockpits." In Human-Computer Interaction. Interaction Modalities and Techniques, 429–38. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-39330-3_45.

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Thomas, Peter, Pradipta Biswas, and Patrick Langdon. "State-of-the-Art and Future Concepts for Interaction in Aircraft Cockpits." In Universal Access in Human-Computer Interaction. Access to Interaction, 538–49. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-20681-3_51.

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Xiong, Duanqin, Qingfeng Liu, Xiaochao Guo, Qingjun Zhang, Qin Yao, Yu Bai, Jian Du, and Yanyan Wang. "The Effect of One-Color and Multi-color Displays with HUD Information in Aircraft Cockpits." In Man-Machine-Environment System Engineering, 389–98. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-2323-1_44.

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Zhu, Hongyu, Xinyang Zhu, Hua Meng, and Yinbo Zhang. "The Accessibility Design and Evaluation of Civil Aircraft Cockpit." In Advances in Ergonomics in Design, 394–99. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-51038-1_54.

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Jovanovic, Mladjan, Dusan Starcevic, and Zeljko Obrenovic. "Designing Aircraft Cockpit Displays: Borrowing from Multimodal User Interfaces." In Transactions on Computational Science III, 55–65. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-00212-0_3.

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Xue, Hongjun, Tao Li, Xiaoyan Zhang, and Rong Wang. "Integrated Usability Evaluation Method for Cockpit of Civil Aircraft." In Lecture Notes in Electrical Engineering, 745–52. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-6232-2_89.

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Suck, Stefan, and Florian Fortmann. "Aircraft Pilot Intention Recognition for Advanced Cockpit Assistance Systems." In Lecture Notes in Computer Science, 231–40. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-39952-2_23.

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Conference papers on the topic "Aircraft cockpits"

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Desjardins, Daniel D., and Darrel G. Hopper. "Military display market segment: aircraft cockpits." In Aerospace/Defense Sensing, Simulation, and Controls, edited by Darrel G. Hopper. SPIE, 2001. http://dx.doi.org/10.1117/12.439136.

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Schabacker, Michael, Moh Sabeur, and Sa´ndor Vajna. "INSIDES: A New Design and Simulation Platform for Virtual Prototyping in Automotive and Aerospace Industry." In ASME 2006 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2006. http://dx.doi.org/10.1115/detc2006-99228.

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Human Machine Interactions Systems (HMI) are decisive for acceptance and safety of new cockpits in the automotive as well as in the aerospace industries. A new design and simulation platform called INSIDES will be presented where virtual cockpit prototypes are being built based on 3D CAD geometry e.g. from CATIA and integrated with logical interaction data derived from UML specifications. This new development platform enables the continuous validation and check of new interaction concepts by involving usability engineers in the very early stage of the development cycle. Since the simulation work is being done in the context of the entire aircraft cockpit / car interior with all instruments, control commands as well as displays devices a better validation of HMI systems can be achieved.
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Feng, Qibin, Yikui Hua, Guoqiang Lv, and Xiaosong Lu. "Thermal stress analysis of laminated LCDs for aircraft cockpits." In 6th International Symposium on Advanced Optical Manufacturing and Testing Technologies (AOMATT 2012), edited by Tianchun Ye, Song Hu, Yanqiu Li, Xiangang Luo, and Xiaoyi Bao. SPIE, 2012. http://dx.doi.org/10.1117/12.977633.

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Hoener, Steven J. "Integration of projection displays into military and commercial aircraft cockpits." In AeroSense 2002, edited by Darrel G. Hopper. SPIE, 2002. http://dx.doi.org/10.1117/12.480922.

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Russell, S. G. "The factors influencing human errors in military aircraft maintenance." In International Conference on People in Control (Human Interfaces in Control Rooms, Cockpits and Command Centres). IEE, 1999. http://dx.doi.org/10.1049/cp:19990198.

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Ge, Lei, Yantao Wang, Huipeng Hu, Lijun Li, and Yiben Zhang. "Numerical Study on Explosion Cutting Process of PMMA Plate and Key Factors Influence on Cutting Performance." In ASME 2018 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/imece2018-86793.

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Polymethylmethacrylate (PMMA) has been widely utilized to manufacture the covers of aircraft cockpits, naval vessels, car windows and so on, due to their high transmittance, low density, easy processing formability, high corrosion resistance and excellent mechanical properties. Under special conditions such as ejection lifesaving, the PMMA plate needs to be split precisely by explosion cutting technology. Hence, an accurate numerical simulation of PMMA structures is significantly important in engineering application. This paper aims to study the cutting behavior of PMMA plate numerically and investigate the influencing factors on cutting performance of PMMA plates. First of all, the simulation of explosion cutting process of PMMA plate is carried out by a non-linear explicit solver in LS-DYNA software using the fluid-solid coupling method. Jones-Wilkins-Lee (JWL) equation of state is used to simulate the relationship between the transient pressure and specific volume of explosives during explosion. The material model considering failure behaviors is used in the simulation. Additionally, the influence of explosive dosage as well as explosive type on the cutting performance of PMMA plate is investigated. Furthermore, the effect of PMMA geometry size on cutting performance is discussed. This study contributes to the knowledge for the design of PMMA structures which needs explosion cutting and the selection of explosive dosage and explosive type.
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Ulbrich, Jr., Erwin A. "Situational awareness in large aircraft." In Cockpit Displays and Visual Simulation, edited by Harry M. Assenheim and Herbert H. Bell. SPIE, 1990. http://dx.doi.org/10.1117/12.20929.

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Doehler, H. U., J. M. Ernst, and Th Lueken. "Virtual aircraft-fixed cockpit instruments." In SPIE Defense + Security, edited by Jack Sanders-Reed and Jarvis J. Arthur. SPIE, 2015. http://dx.doi.org/10.1117/12.2177796.

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Aygün, Mehmet Murat, Yiğit Tascıoğlu, Gürsoy Genç, and Mustafa Altunay. "Electro-Mechanical Control Loading System for Rotary Wing Aircraft Simulators." In ASME 2014 12th Biennial Conference on Engineering Systems Design and Analysis. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/esda2014-20495.

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The focus of this paper is on the development of a high-fidelity electro-mechanical Control Loading System (CLS) for a rotary wing aircraft simulator. CLS is one of the major components of a flight simulator. It is used for providing realistic force feedback to pilots. The pilot in a real aircraft feels the forces acting on control surfaces through cockpit controls. During simulation, these forces are produced by CLS actuators. For this reason, CLS must behave exactly like the aircraft control hardware, statically and dynamically. The fidelity of the force feel simulation is a key criterion for flight simulation certification. It is also important that a CLS design is reconfigurable and modular such that it conforms easily to different simulator models and simulations of different aircrafts. The work also includes system integration of a research simulator for testing purposes. Design and selection of hardware and software components of the CLS and the simulator are presented along with the overall system architecture.
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Jennings, Randle, and Larry Hannert. "Human Factors Associated with Glass Cockpit Design." In General Aviation Aircraft Meeting and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1987. http://dx.doi.org/10.4271/871036.

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Reports on the topic "Aircraft cockpits"

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Zehner, Gregory F. Prediction of Anthropometric Accommodation in Aircraft Cockpits. Fort Belvoir, VA: Defense Technical Information Center, June 2001. http://dx.doi.org/10.21236/ada399750.

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2

Rash, C., C. Suggs, P. LeDuc, G. Adam, and S. Manning. Accident Rates in Glass Cockpit Model U.S. Army Rotary-Wing Aircraft. Fort Belvoir, VA: Defense Technical Information Center, August 2001. http://dx.doi.org/10.21236/ada396085.

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Hicks, Jamison S., and David B. Durbin. An Investigation of Multiple Unmanned Aircraft Systems Control from the Cockpit of an AH-64 Apache Helicopter. Fort Belvoir, VA: Defense Technical Information Center, December 2014. http://dx.doi.org/10.21236/ada616169.

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