Considerations regarding the composition of the cockpit view for a modern simulator

Q2 Engineering
Anton BALABAN, Andrei NEAMTU, Sorin BERBENTE, Gabriela-Liliana STROE, Irina-Beatrice STEFANESCU, Emil COSTEA, Irina-Carmen ANDREI, Ionel POPESCU
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引用次数: 0

Abstract

This study shows how to generate images and compose images in the modern simulator room by starting multiple work sessions running at the same time so that all active server stations and the station to connect to are continuously displayed. Each server handles specific functions of the simulation process and runs a dedicated software application for its specific functions. For a supervised flight simulator, the following functions need to have dedicated applications: 1) Flight Dynamics Simulation, 2) Graphical projection, 3) Cockpit and Flight instrumentation simulation and integration, 4) Supervisor station. Out of these functions, Graphical projections and Cockpit and Flight instrumentation and integration require the most computational resources. Simulators need to present the view from a cockpit which requires a field of view of at least 180 degrees. This requires at least three displays usually in the form of projectors. In legacy implementations due to computational bottlenecks, each projector needed a dedicated computer. Similarly, the Cockpit and Flight instrumentation simulation requires usually upwards of 100 flight instrument simulations and embedded processors to be managed. In legacy implementations, one computer is needed for each piloting station. In recent implementations due to the increased performance of multi-core processors, many of these functions can be handled by single computers: the flight dynamics simulation and graphical projection functions can currently be handled by a single computer, similarly, all Cockpit and Flight instrumentation simulation and integration can be handled by another computer. Thus, a minimum of three servers are required to ensure full functionality of supervised simulation using modern computing systems.
关于现代模拟器座舱视图组成的考虑
本研究展示了如何在现代模拟室内通过启动同时运行的多个工作会话来生成图像和组合图像,以便连续显示所有活动的服务器站和要连接的站。每个服务器处理模拟过程的特定功能,并为其特定功能运行专用软件应用程序。对于监督飞行模拟器,以下功能需要有专门的应用:1)飞行动力学仿真,2)图形投影,3)驾驶舱和飞行仪表仿真与集成,4)监督员站。在这些功能中,图形投影、座舱和飞行仪表以及集成需要最多的计算资源。模拟器需要呈现驾驶舱的视图,这需要至少180度的视野。这需要至少三个显示器,通常以投影仪的形式。在传统的实现中,由于计算瓶颈,每个投影仪都需要一台专用计算机。类似地,驾驶舱和飞行仪表模拟通常需要超过100个飞行仪表模拟和嵌入式处理器来管理。在传统的实现中,每个引航站需要一台计算机。在最近的实现中,由于多核处理器的性能提高,许多这些功能可以由单台计算机处理:飞行动力学仿真和图形投影功能目前可以由单台计算机处理,类似地,所有驾驶舱和飞行仪表的仿真和集成可以由另一台计算机处理。因此,至少需要三个服务器来确保使用现代计算系统的监督模拟的全部功能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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