Relevant bibliographies by topics / Cockpit Display System

Contents

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

Academic literature on the topic 'Cockpit Display System'

Author: Grafiati
Published: 4 June 2021
Last updated: 13 February 2022

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Journal articles on the topic "Cockpit Display System"

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TORY, Makoto, and Yoichiro KURIHARA. "Cockpit Display System." Journal of the Japan Society for Aeronautical and Space Sciences 45, no. 524 (1997): 507–10. http://dx.doi.org/10.2322/jjsass1969.45.507.

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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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Theunissen, Erik, and Tim Etherington. "Computer graphics in the cockpit." Information Design Journal 11, no. 1 (September 26, 2003): 4–16. http://dx.doi.org/10.1075/idj.11.1.03the.

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Spatially integrated data presentation for electronic flight displays was first proposed over forty years ago. Yet, in current state-of-the-art cockpits, only 2-D instruments are depicted on the electronic displays. The first part of this paper will discuss today’s state-of-the-art in 3-D computer graphics in relation to the graphics used in today’s electronic flight displays and illustrate how properties of the display medium, system requirements, image generation capabilities and current practices influence the design. The second part will discuss the design rationale behind a synthetic vision display format in the light of the requirements and constraints.
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Read, B. C. "Developing the next generation cockpit display system." IEEE Aerospace and Electronic Systems Magazine 11, no. 10 (1996): 25–28. http://dx.doi.org/10.1109/62.538798.

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Hayashi, Miwa, Valerie Huemer, Fritz Renema, Steve Elkins, Jeffrey W. McCandless, and Robert S. McCann. "Effects of the Space Shuttle Cockpit Avionics Upgrade on Crewmember Performance and Situation Awareness." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 49, no. 1 (September 2005): 54–58. http://dx.doi.org/10.1177/154193120504900113.

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The Space Shuttle Cockpit Avionics Upgrade (CAU) is a proposed cockpit display upgrade designed to address human-factors usability issues of the current suite of cockpit displays, Multifunction Electronic Display System (MEDS). Unlike MEDS, CAU consolidates information in a task-oriented manner, rather than a data-source-oriented manner. CAU also makes greater use of color coding and graphical depictions in systems status presentations. An ascent-phase operation simulation study showed that CAU formats significantly improved the participants' abort-related situation awareness. Participants also performed certain malfunction management procedures more accurately when CAU was used. The Space Shuttles are now scheduled to be retired by 2010 without incorporating CAU; however, the results of the present study suggest that the human-centered design concepts are effective and can be extended to the cockpit interface design of NASA's next generation Crew Exploration Vehicle.
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Liu, Jian, Yan Ran Wang, and Wei Jie Zhao. "Cockpit Display System Simulation of General Aviation Aircraft Based on VAPS XT." Advanced Materials Research 846-847 (November 2013): 1893–98. http://dx.doi.org/10.4028/www.scientific.net/amr.846-847.1893.

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This paper introduces a recent study of Cockpit Display System (CDS) simulation for general aviation aircraft. The cockpit display simulation system is developed for avionics system integration and test by using VAPS XT software. This paper describes the cycle of developing human-machine interfaces (HMI) with VAPS XT, designs the Primary Flight Display (PFD) and Multi-functional Display (MFD) interfaces based on system requirements, and analyzes key technologies in the simulation process. The simulation result is proved to have good real-time effect and high fidelity and the simulation system has gained favorable effects in the exploitation of a practical avionics project.
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Liu, Wei, Cheng Kun Liu, Da Min Zhuang, Zhong Qi Liu, and Xiu Gan Yuan. "The Evaluation Method of Mental Workload on Visual Interface in Cockpit." Advanced Materials Research 433-440 (January 2012): 6477–82. http://dx.doi.org/10.4028/www.scientific.net/amr.433-440.6477.

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Objective to establish a system to evaluate the mental workload on visual display interface in airplane cockpit after synthesizing three kinds of mental workload assessment techniques, i.e. main task measure method, physiology measure method and subjective evaluate method. Methods The evaluation indices of every kind of assessment techniques was defined, and the amount of each index through experiment and subjective inquiry was gained, weighted average was calculated and a quantification evaluation value of each kind of evaluation methods was got. At last, with weighted calculation of above three evaluation values, the evaluation value of mental workload on visual display interface in airplane cockpit was obtained Results in M kinds of different designs of visual display interface in airplane cockpit, the synthetic evaluation value of one design was the smallest and the mental workload of this design was the smallest. The design of the smallest mental workload was chosen prior as the final scheme of visual display interface in airplane cockpit .Conclusion The evaluation system is combined with present main evaluation methods of mental workload and utilizes their advantages. The evaluating results can be quantified more directly and clearly. With this evaluation system, the mental workload can be evaluated during the design of visual display interface of airplane cockpit and the best scheme can be confirmed.
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Danilov, S., M. Kozyrev, M. Grechanichenko, L. Grodzitskiy, V. Mizginov, and V. V. Kniaz. "SYNTHETIC VISION SYSTEM CALIBRATION FOR CONFORM PROJECTION ON THE PILOT’S HEAD-UP DISPLAY." ISPRS - International Archives of the Photogrammetry, Remote Sensing and Spatial Information Sciences XLIII-B2-2020 (August 12, 2020): 575–81. http://dx.doi.org/10.5194/isprs-archives-xliii-b2-2020-575-2020.

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Abstract. Situational awareness of the crew is critical for the safety of the air flight. Head-up display allows providing all required flight information in front of the pilot over the cockpit view visible through the cockpit’s front window. This device has been created for solving the problem of informational overload during piloting of an aircraft. While computer graphics such as scales and digital terrain model can be easily presented on the such display, errors in the Head-up display alignment for correct presenting of sensor data pose challenges. The main problem arises from the parallax between the pilot’s eyes and the position of the camera. This paper is focused on the development of an online calibration algorithm for conform projection of the 3D terrain and runway models on the pilot’s head-up display. The aim of our algorithm is to align the objects visible through the cockpit glass with their projections on the Head-up display. To improve the projection accuracy, we use an additional optical sensor installed on the aircraft. We combine classical photogrammetric techniques with modern deep learning approaches. Specifically, we use an object detection neural network model to find the runway area and align runway projection with its actual location. Secondly, we re-project the sensor’s image onto the 3D model of the terrain to eliminate errors caused by the parallax. We developed an environment simulator to evaluate our algorithm. Using the simulator we prepared a large training dataset. The dataset includes 2000 images of video sequences representing aircraft’s motion during takeoff, landing and taxi. The results of the evaluation are encouraging and demonstrate both qualitatively and quantitatively that the proposed algorithm is capable of precise alignment of the 3D models projected on a Head-up display.
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Gao, Jing, Yin Liang Jia, and Bing Yang Li. "The Integrated Display System in Aircraft Cockpit Based on FPGA." Applied Mechanics and Materials 651-653 (September 2014): 911–15. http://dx.doi.org/10.4028/www.scientific.net/amm.651-653.911.

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The main research object is the graphics generation and display system based on FPGA, the system is mainly used for the integrated display of aircraft cockpit. The display system has the characteristics of large amount of data, real-time processing in the graphics generation. According to the characters, the paper uses programmable logic device due to FPGA has the advantages of high speed, real time. In order to further improve the efficiency of the system, the paper also designs the ping-pong operation of double SSRAM(Synchronous Static Random Access Memory) at the same time. Through the experiment, the system can run well and achieve the desired objectives.
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Hettinger, Lawrence J., Bart J. Brickman, Merry M. Roe, W. Todd Nelson, and Michael W. Haas. "Effects of Virtually-Augmented Fighter Cockpit Displays on Pilot Performance, Workload, and Situation Awareness." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 40, no. 2 (October 1996): 30–33. http://dx.doi.org/10.1177/154193129604000205.

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Virtually-augmented display concepts are being developed at the US Air Force Armstrong Laboratory's Synthesized Immersion Research Environment (SIRE) Facility at Wright-Patterson Air Force Base, Ohio, for use in future USAF crew stations. These displays incorporate aspects of virtual environment technology to provide users with intuitive, multisensory representations of operationally relevant information. This paper describes an evaluation that was recently conducted to contrast the effects of conventional, F-15 types of cockpit displays and virtually-augmented, multisensory cockpit displays on pilot-aircraft system performance, workload, and situation awareness in a simulated air combat task. Eighteen military pilots from the United States, France, and Great Britain served as test pilots. The results indicate a statistically significant advantage for the virtually-augmented cockpit configuration across all three classes of measures investigated. The results are discussed in terms of their relevance for the continuing evolution of advanced crew station design.
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Dissertations / Theses on the topic "Cockpit Display System"

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Portnoy, Michael, and Albert Berdugo. "AN XML-DRIVEN ARCHITECTURE FOR INSTRUMENTATION COCKPIT DISPLAY SYSTEMS." International Foundation for Telemetering, 2005. http://hdl.handle.net/10150/604885.

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ITC/USA 2005 Conference Proceedings / The Forty-First Annual International Telemetering Conference and Technical Exhibition / October 24-27, 2005 / Riviera Hotel & Convention Center, Las Vegas, Nevada
Designing and implementing an instrumentation cockpit display system presents many unique challenges. The system must be easy to use, yet highly customizable. Typically, these systems require an experienced programmer to create graphical display screens. Furthermore, most current display systems do not provide for bi-directional communication between the instrumentation system and the display system. This paper discusses an architecture that addresses these issues and other common problems with cockpit displays. This system captures data from the instrumentation system, displays parameters, and returns calculated parameters and status information regarding pilot actions to the instrumentation system. Unlike traditional systems, the configuration of the graphical presentation of the cockpit display can be done by a non-programmer. All communication between the instrumentation system and the cockpit display system is done transparently using XML. The usage of XML in this system facilitates real-time form previewing, cross-platform compatibility, and seamless transitions between project management, graphical configuration, and engineering unit conversions.
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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 using custom made user interface system design tool.
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Chinthammit, Winyu. "Hybrid inertial-laser scanning head tracking system for cockpit applications /." Thesis, Connect to this title online; UW restricted, 2007. http://hdl.handle.net/1773/5972.

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Norén, Johan. "Warning systems design in a glass cockpit environment." Thesis, Linköping University, Department of Management and Engineering, 2008. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-11092.

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In Sweden close to 500 people are killed and several thousands severely injured in traffic each year. This is one of the largest health problems for society in both Sweden and the whole world. In the cars of tomorrow will the main instrument panel and the centre console be screen-based instead of the current solution with “iron instruments” and other physical devices. This future driver environment opens for a flexible and situation-dependent usage of presentation resources. The purpose of this thesis is to explore these possibilities from a warning system perspective.

The project had its main focus on designing warning system concepts using the HUD and vibrotactile information in a coordinated way based on established HMI principles. Another goal for this thesis work was to generate a functional concept for demonstration and evaluation in the virtual reality lab at the University of Linköping.

The method of realization was divided into three phases – information gathering, concept generation and implementation. These phases are commonly used in design projects. This way of work supplies structure to the project and makes it possible to achieve an iterative design process.

The information gathering involved a thorough theoretical study of HMI, interface design and warning design. A state of the art investigation was then conducted to find out how the warning systems, relevant to this thesis, are presented today.

The concept generation was divided into two parts – warning system design and visual design. The Warning system design concepts were based on different combinations from a morphologic matrix and relevant theory. Consideration was also taken to when the systems are likely to be activated and which modality, or modalities, that then was suitable to use. The visual design concepts were developed by using creative product development methods and the iterative Simulator-Based Design (SBD) theory.

After concluding the concept generation was the visual design results given functionality by programming software. The visual warning system were then integrated in the simulator software and fully implemented in the simulator cockpit at the university.

The implemented warning systems were then evaluated by a pilot study conducted in the simulator. Test persons were invited to the VR-lab and given an introduction to the warning systems. They were then asked to drive a predetermined route with a number of different warning system conditions. These test results were later statistically analyzed and evaluated.

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Bílek, Jan. "Aerospace - Futuristický kokpit moderního letounu." Master's thesis, Vysoké učení technické v Brně. Fakulta informačních technologií, 2010. http://www.nusl.cz/ntk/nusl-237164.

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This work describes the visualization design of the flight related quantities in a cockpit of a modern light sport aircraft. It focuses on the utilization of the state of the art trends in flight data displays and introduces the innovative implementation of the aircraft's energy state smart clues that reduce pilots' workload. The initial part of the work presents a research into the flight, engine and navigation data presentation on analog instruments, followed by their illustrative depiction in glass cockpits. Within the framework of this thesis, Microsoft Flight Simulator has been used as a source of the flight related data. Final advances in the display design were introduced through the implementation of the synthetic vision system and a visualization of the virtual tunnel in the sky.
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Yankosky, Leonard Joseph. "Investigating the role of procedures and cockpit display of traffic information in candidate air traffic management operations." Thesis, Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/21616.

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Palmer, Ryan C. "Applying Human Factors Principles In Aviation Displays: A Transition From Analog to Digital Cockpit Displays In The CP140 Aurora Aircraft." 2007. http://trace.tennessee.edu/utk_gradthes/185.

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A flight test program that evaluated the results of a CP140 Aurora cockpit modernization project was conducted between May 2004 and October 2005. This paper uses the results of that test program to show how basic human factors principles were violated which led to the identification of multiple design deficiencies. This paper proposes that the failure to apply good human factors principles when designing aircraft displays can lead to unacceptable deficiencies. The result can be poor modal awareness, confusion in the cockpit, and often negative training for the pilots. In particular, four major deficiencies were analyzed to determine the specific human factors principles that were breached. The violations included a lack of concise and relevant feedback to the pilot, unclear and ambiguous annunciations, poor use of colour coding principles and logic, a lack of suitable attention capture cueing, inappropriate alert cueing, an absence of aural cueing during specific degraded modes of operation, excessive cognitive workload, and a failure to incorporate the pilot as the focal point of the display design, also known as a human centred design philosophy. Recommendations for system design enhancements are provided to ensure safe and effective operations of this prototype system prior to operational implementation. The evaluation of the prototype system design was conducted by a flight test team from the Aerospace Engineering Test Establishment in Cold Lake, Alberta and supported by the Maritime Proving and Evaluation Unit in Greenwood, Nova Scotia. The test program encompassed a thorough review of system design documentation, abinitio training and preliminary testing in a Systems Integration Lab and 40 flight test missions. The recorded deficiencies were based upon the observations of two Qualified Test Pilots.
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Books on the topic "Cockpit Display System"

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Franklin, James A. Collaborative research on V/STOL control system/cockpit display tradeoffs under the NASA/MOD joint aeronautical program. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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Franklin, James A. Collaborative research on V/STOL control system/cockpit display tradeoffs under the NASA/MOD joint aeronautical program. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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Williams, Kevin W. Usability and effectiveness of advanced general aviation cockpit displays for instrument flight procedures. Washington, D.C: Office of Aerospace Medicine, Federal Aviation Administration, 2003.

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Bud, Melissa. Terrain display alternatives: Assessment of information density and alerting strategies. Washington, D.C. (800 Independence Ave. S. W. Washington 20591): The Department, Office of Aviation Research, 1998.

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

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Prinzo, O. Veronika. Automatic Dependent Surveillance-Broadcast/cockpit display of traffic information: Innovations in aircraft navigation on the airport surface. Washington, D.C: U.S. Federal Aviation Administration, Office of Aerospace Medicine, 2004.

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Jones, Denise R. Simulator comparison of thumball, thumb switch and touch screen input concepts for interaction with a large screen cockpit display format. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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Aerospace Behavioral Engineering Technology Conference (6th 1987 Long Beach, Calif.). Sixth Aerospace Behavioral Engineering Technology Conference proceedings: "human/computer technology : who's in control?". Warrendale, PA: Society of Automotive Engineers, 1988.

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Aerospace, Behavioral Engineering Technology Conference (5th 1986 Long Beach Calif ). Fifth Aerospace Behavioral Engineering Technology Conference proceedings: "human integration technology, the cornerstone for enhancing human performance". Warrendale, PA: Society of Automotive Engineers, 1987.

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Book chapters on the topic "Cockpit Display System"

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Xue, Hong-jun, Xiu-bo Yu, and Xiao-yan Zhang. "Usability Evaluation of the Cockpit Display System." In Design, User Experience, and Usability: Novel User Experiences, 655–62. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-40355-7_63.

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Heng-yang, Wei, Zhuang Da-min, and Wan-yan Xiao-ru. "Simulation of a Cockpit Display System under the Sunlight." In Advances in Intelligent and Soft Computing, 411–16. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-28308-6_56.

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Bai, Qingyuan, Yang Bai, Xinglong Wang, Xingmei Zhao, and Jin Yu. "Ergonomics Index System of Airplane Cockpit Display and Control Resources." In Advances in Intelligent Systems and Computing, 827–32. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-11051-2_126.

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Xue, Hongjun, Tao Li, and Xiaoyan Zhang. "An Approach for Assessing the Usability of Cockpit Display System." In Engineering Psychology and Cognitive Ergonomics: Cognition and Design, 317–25. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-58475-1_24.

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Wu, Huaxing, Kai Qiu, Wei Huang, and Fengju Kang. "Extensible Software Architecture for Simulating Cockpit Display and Control System." In Proceedings of the 2013 International Conference on Electrical and Information Technologies for Rail Transportation (EITRT2013)-Volume I, 501–10. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-53778-3_49.

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Wang, Yanyan, Qingfeng Liu, Wanli Lou, Duanqin Xiong, Yu Bai, Jian Du, and Xiaochao Guo. "Ergonomics Evaluation of Large Screen Display in Cockpit Based on Eye-Tracking Technology." In Man-Machine-Environment System Engineering, 347–56. Singapore: Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-2481-9_40.

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Wang, Lijing, Yanzeng Zhao, and Yu Zhu. "Construction of Ergonomic Evaluation System for Display and Control Characteristics of Aircraft Cockpit Touch Panel." In Lecture Notes in Electrical Engineering, 577–84. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-16-5963-8_79.

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Dyachenko, Sergey Aleksandrovich, Dmitry Mikhailovich Ilyashenko, and Evgeny Sergeevich Neretin. "The Automation Tool Development for Aircraft Cockpit Display Systems Verification in Part of Text Data." In Lecture Notes of the Institute for Computer Sciences, Social Informatics and Telecommunications Engineering, 329–35. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-67514-1_26.

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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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Davis, Bradley M., Kelly Dickerson, and Samineh C. Gillmore. "User Centered Design Strategies for Improving Visualization of Sensor Data in Rotorcraft Cockpit Displays for Degraded Visual Environment Operations." In Advances in Intelligent Systems and Computing, 131–41. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-19135-1_13.

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Conference papers on the topic "Cockpit Display System"

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Bailey, David C. "F-22 cockpit display system." In SPIE's International Symposium on Optical Engineering and Photonics in Aerospace Sensing, edited by Darrel G. Hopper. SPIE, 1994. http://dx.doi.org/10.1117/12.177777.

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Quick, John R. "System requirements for a high-gain dome-display surface." In Cockpit Displays and Visual Simulation, edited by Harry M. Assenheim and Herbert H. Bell. SPIE, 1990. http://dx.doi.org/10.1117/12.20945.

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Wan, Huagen, Song Zou, Zilong Dong, Hai Lin, and Hujun Bao. "MRStudio: A mixed reality display system for aircraft cockpit." In 2011 IEEE International Symposium on VR Innovation (ISVRI). IEEE, 2011. http://dx.doi.org/10.1109/isvri.2011.5759615.

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Yuan, Mei, and Jiong Chen. "Design and optimization of virtual cockpit integrated display system." In Sixth International Symposium on Instrumentation and Control Technology: Sensors, Automatic Measurement, Control, and Computer Simulation, edited by Jiancheng Fang and Zhongyu Wang. SPIE, 2006. http://dx.doi.org/10.1117/12.718216.

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Zhou Yingwei, Zhuang Damin, Zhang Lei, and Wanyan Xiaoru. "Study on ergonomics evaluation method of the cockpit display system." In 2010 IEEE 11th International Conference on Computer-Aided Industrial Design & Conceptual Design 1. IEEE, 2010. http://dx.doi.org/10.1109/caidcd.2010.5681276.

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Wang, Zhile, XU Luhang, HU Wenting, and SUN Zhongyun. "Research on graphic generation technology of airborne cockpit display system." In Eleventh International Conference on Graphics and Image Processing, edited by Zhigeng Pan and Xun Wang. SPIE, 2020. http://dx.doi.org/10.1117/12.2558056.

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Brandtberg, Hans. "JAS 39 cockpit display system and development for the future." In SPIE's 1995 Symposium on OE/Aerospace Sensing and Dual Use Photonics. SPIE, 1995. http://dx.doi.org/10.1117/12.210953.

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Campbell, Steven, Robert Grappel, Michael Hoffman, Richard Hogaboom, Richard Lloyd, and John O'Rourke. "Corridor Integrated Weather System (CIWS) Cockpit Weather Display Data Link Demonstration." In AIAA Guidance, Navigation, and Control Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-4930.

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Барладян, Борис, Boris Barladyan, Лев Шапиро, Lev Shapiro, Курбан Маллачиев, Kurban Mallachiev, Алексей Хорошилов, et al. "Multi-windows Rendering Using Software OpenGL in Avionics Embedded Systems." In 29th International Conference on Computer Graphics, Image Processing and Computer Vision, Visualization Systems and the Virtual Environment GraphiCon'2019. Bryansk State Technical University, 2019. http://dx.doi.org/10.30987/graphicon-2019-2-28-31.

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Elaboration of modern airplane cockpit has tendency to use large displays instead of a lot of separate indicators. The large display should combine information about flight navigation and state of plane equipment. Information coming from a wide variety of devices should be displayed simultaneously. Therefore multi-windows rendering is vitally important here. Its implementation must be embedded in real-time operating system which controls the aircraft. Development of a Safety Critical Compositor for multi-windows rendering for OpenGL SC 1.0.1 software is considered in the paper. It works under the real-time operating system JetOS newly designed for aircraft. Development is based on the use of extensions designed to work in multi-core systems in addition to standard JetOS partitioning services.
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Muto, Yasuaki. "Evolution of in-vehicle display technology and Innovation of the cockpit system." In 2018 25th International Workshop on Active-Matrix Flatpanel Displays and Devices (AM-FPD). IEEE, 2018. http://dx.doi.org/10.23919/am-fpd.2018.8437393.

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Reports on the topic "Cockpit Display System"

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Davis, Lawrence, Betsy Constantine, Stuart Shieber, Joe Marks, and Rebecca Hwa. Optimizing Cockpit Display Configurations with a Genetic Algorithm System. Phase 1. Fort Belvoir, VA: Defense Technical Information Center, December 1994. http://dx.doi.org/10.21236/ada289799.

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