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Journal articles on the topic 'Flight simulator'

Author: Grafiati

Published: 4 June 2021

Last updated: 25 July 2025

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1

Oh, Chang-Geun. "Pros and Cons of A VR-based Flight Training Simulator; Empirical Evaluations by Student and Instructor Pilots." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 64, no. 1 (2020): 193–97. http://dx.doi.org/10.1177/1071181320641047.

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A medium-fidelity virtual reality (VR) flight simulator was developed to evaluate how aircraft pilots perceived simulated flights in the VR environment compared with conventional mockup-based simulators. In Experiment 1, student and instructor pilots conducted ten repeating flights in the simulator. Three extreme flight conditions were created, and participants rated perceptions of the extreme flights using multiple criteria. In Experiment 2, pilots manipulated G1000 electronic cockpit systems in the simulator during three repeating simulated flights and were asked to rate their perceptions of

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Kennedy, R. S., G. O. Allgood, B. W. Van Hoy, and M. G. Lilienthal. "Motion Sickness Symptons and Postural Changes following Flights in Motion-Based Flight Trainers." Journal of Low Frequency Noise, Vibration and Active Control 6, no. 4 (1987): 147–54. http://dx.doi.org/10.1177/026309238700600402.

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Navy pilots flew over 193 standard training mission scenarios while acceleration recordings in three linear dimensions (gx, gy, and gz) were made for two moving-base flight trainers. The pilots, who were of comparable age and experience in both groups, were interviewed for motion sickness symptomatology and were tested for ataxia after leaving the simulators. The aircraft simulated included a P-3C turboprop fixed-wing patrol aircraft (2F87F), and an SH-3 antisubmarine warfare helicopter (2F64C). Motion sickness incidence was high in the SH-3 simulator and nonexistent in the P-3C. Ataxia scores

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Prayitno, Hadi, Ekohariadi, Mochamad Cholik, Lilik Anifah, Arie Wardhono, and Putra Wicaksono. "Improving Pilot Competence Through Flying Practice Learning Using Flight Simulator at the Indonesia Civil Pilot Academy of Banyuwangi." Journal of Law and Sustainable Development 12, no. 1 (2024): e2426. http://dx.doi.org/10.55908/sdgs.v12i1.2426.

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Objective: Indonesia Pilot Academy of Banyuwangi uses simulators to improve pilots' capabilities and maintain their skills. The pilot training process includes theoretical study, flight simulator and practical training. A total of eight simulators are available, including two ALSIMs and three each of the Redbird TD2 and FMX 1000. Using a simulator reduces the risk of flying in realistic conditions. Therefore, the purpose of this study is to measure the degree of effectiveness of practical flight learning, assess students' perceptions of practical flight learning, and analyze the impact of prac

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Stein, Michael, and Maxi Robinski. "Simulator Sickness in Flight Simulators of the German Armed Forces." Aviation Psychology and Applied Human Factors 2, no. 1 (2012): 11–19. http://dx.doi.org/10.1027/2192-0923/a000022.

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We investigated simulator sickness in jet simulators without motion platforms (Eurofighter), and in a helicopter simulator (EC 135) as well as in a reconnaissance aircraft simulator (P-3C-Orion) with motion simulation. In addition, workload, visual fatigue, and vitality of pilots were measured. In contrast to jet simulators, where no flashbacks were reported, the EC 135 and the P-3C-Orion simulators proved to be problematic, causing severe simulator sickness symptoms or flashbacks. In all three studies, simulator sickness correlated positively with workload and visual fatigue, while correlatin

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Williams, S. Tyler, Adrienne M. Madison, and Valeta Carol Chancey. "A Biomechanical Investigation of Cervical Spine Range of Motion for UH-60 Aviators in Real and Simulated Flight Environments." Military Medicine 188, Supplement_6 (2023): 240–45. http://dx.doi.org/10.1093/milmed/usad101.

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ABSTRACT Introduction Military flight surgeons evaluating aviators for flight fitness based on the cervical spine range of motion (CROM) have no operationally relevant reference with which to make a reliable determination. The published physiological limits for the general population do not necessarily apply to military aviators. CROM requirements for rotary-wing aviators would ideally be defined by measurements taken directly within their operational environment. Materials and Methods Nine subjects performed the same predetermined 1-hour flight mission in a UH-60 aircraft and then, at least 2

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Andrienko, Oleksandr, Mykola Huchenko, Volodymyr Zinchenko, and Oleksandr Zhorniak. "SOFTWARE-HARDWARE COMPLEX OF QUALIFICATION EVALUATION OF MI-171 HELICOPTER SIMULATOR." TECHNICAL SCIENCES AND TECHNOLOGIES, no. 3(17) (2019): 49–54. http://dx.doi.org/10.25140/2411-5363-2019-3(17)-49-54.

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Urgency of the research. Flight safety is an actual practical issue which solving influences the future of Ukraine as a transport state. As a consequence of technical progress aviation technology is becoming more and more sophisticated and reliable. However, the intensity of the impact on a person caused by various adverse factors, including information overloads, is constantly increasing. Statistics show that up to 80% of accidents and disasters occur due to pilot errors. The reason for about 35 % of these errors is lack of professional training, and about 40% of the errors are caused by inex

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Kumar, P. Suresh, and K. Senthil Kumar. "Airborne Sensor Model Position Fidelity Determination for Combat Aircraft Simulators." Advanced Materials Research 1016 (August 2014): 429–35. http://dx.doi.org/10.4028/www.scientific.net/amr.1016.429.

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Airborne sensors become a primary system in any combat program and the effectiveness depends on the coverage spectrum of the sensors and also the ability of flying machine. However evaluating the mission functionalities using sensors in flight involves tasks namely, Man Machine interface evaluation, Sensor function capability evaluation, System interface evaluation, Performance evaluation, pilot work load etc needs to carried out and the issues observed during the flight test needs to be cleared before accepting the system. It is one of the challenging task for any combat aircraft development

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8

Tarricone, Paul. "Flight Simulator." Lighting Design + Application 40, no. 9 (2010): 49–52. https://doi.org/10.1177/036063251004000912.

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9

C, Rachel. "Flight Simulator." Scientific American 320, no. 6 (2019): 17. http://dx.doi.org/10.1038/scientificamerican0619-17.

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Park, Seongjoon, Woong Gyu La, Woonghee Lee, and Hwangnam Kim . "Devising a Distributed Co-Simulator for a Multi-UAV Network." Sensors 20, no. 21 (2020): 6196. http://dx.doi.org/10.3390/s20216196.

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Practical evaluation of the Unmanned Aerial Vehicle (UAV) network requires a lot of money to build experiment environments, which includes UAVs, network devices, flight controllers, and so on. To investigate the time-sensitivity of the multi-UAV network, the influence of the UAVs’ mobility should be precisely evaluated in the long term. Although there are some simulators for UAVs’ physical flight, there is no explicit scheme for simulating both the network environment and the flight environments simultaneously. In this paper, we propose a novel co-simulation scheme for the multiple UAVs networ

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11

Allerton, D. J. "Flight simulation - past, present and future." Aeronautical Journal 104, no. 1042 (2000): 651–63. http://dx.doi.org/10.1017/s0001924000096901.

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Abstract This paper outlines the development of flight simulators used in civil training, military training and in engineering simulation. It describes the evolution of flight simulators and the typical architecture of a modern flight simulator. The technical innovations, which have occurred in modelling, motion systems and visual systems are reviewed. The paper also reviews the transfer of training in flight simulation, the application of simulation to engineering design and outlines problems which are encountered in flight simulation. The paper concludes by reviewing the current trends in fl

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Perfect, P., M. D. White, G. D. Padfield, and A. W. Gubbels. "Rotorcraft simulation fidelity: new methods for quantification and assessment." Aeronautical Journal 117, no. 1189 (2013): 235–82. http://dx.doi.org/10.1017/s0001924000007983.

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AbstractFlight simulators are integral to the design/development, testing/qualification, training and research communities and their utilisation is ever expanding. The use of flight simulation to provide a safe environment for pilot training, and in research and development, must be underpinned by quantification of simulator fidelity. While regulatory simulator standards exist for flight training simulators and new standards are in development, previous research has shown that current standards do not provide a fully quantitative approach for assessing simulation fidelity, especially in a rese

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Kabanyachyi, Volodymyr, and Beycan Ibrahimoglu. "Problem of low-frequency motion cueing along roll on flight simulators." MECHANICS OF GYROSCOPIC SYSTEMS, no. 48 (December 26, 2024): 81–91. https://doi.org/10.20535/0203-3771482024317962.

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An innovative approach to improve the fidelity of low-frequency lateral motion cueing within full-flight simulators for non-maneuvering aircraft is presented. On the basis of the perception peculiarities by the human vestibular system of movement along the roll, the problem of low-frequency motion cueing of lateral movement by motion systems of flight simulators was formulated and solved. The critical challenge of simulating the set of angular motion cues that pilots perceive during flights is decided. This research highlights two key outcomes. The fourth-order low-pass filter effectively extr

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Zhang, Ya Ni, Yan Li, and Ya Kui Gao. "Commercial Transport Aircraft Flight Simulator Flying Qualities Airworthiness Verification." Applied Mechanics and Materials 235 (November 2012): 170–75. http://dx.doi.org/10.4028/www.scientific.net/amm.235.170.

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Flight simulation is a simulation of flight and various aspects of the flight environment. Flight simulation is used for a variety of reasons, including aircraft development and flight training. The engineering flight simulator is used for a certain commercial transport aircraft development. The aircraft adopts fly-by-wire flight control technology. The engineering flight simulator was mainly used as a platform to test flying quality of the aircraft. The simulator has actual aircraft cockpit with wide-field visual system mounted on large six degree of freedom(DOF) motion platform that feature

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Xiao, Zhi Jian, and Jiang Jun Xu. "Simulation and Design of Control and Display Unit for Full Flight Simulator." Applied Mechanics and Materials 526 (February 2014): 273–76. http://dx.doi.org/10.4028/www.scientific.net/amm.526.273.

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In order to solve the problem of simulation difficulty of the control and display unit (CDU) for full flight simulator, it is real significance to design the CDU. The principles and design methods are expounded about the CDU in detail. The simulation CDU is tested on full flight simulator. The results show that the simulation CDU can establish flight plan, modify flight route, and set the performance parameters. The component has correct logic, high fidelity and reliable performance. The simulation CDU can meet full flight simulator design requirements.

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Sheng, Xiao Wei, Jun Wei Han, and Ming Hui Hao. "Sound Analysis and Synthesis for Audio Simulation System of Flight Simulator." Advanced Materials Research 748 (August 2013): 708–12. http://dx.doi.org/10.4028/www.scientific.net/amr.748.708.

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Through simulating the feelings of vision, hearing, motion and force during flight, the flight simulator can build a realistic flight environment on the ground. Therefore, Flight simulators have an important role in pilot training field. Audio simulation system is a key component of the flight simulator, it has direct impact on the realism and immersion of flight simulation. In this paper, we introduced the development procedure of audio simulation system shortly. Software implementation and its key development technology were mainly focused for expressing the necessity of extracting sound sou

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Luo, Peng, Ronghua Hu, Junlin Bai, and Yang Shu. "Research into the kinematic singularity problem of an all-attitude simulator and its control." Transactions of the Canadian Society for Mechanical Engineering 46, no. 1 (2022): 132–39. http://dx.doi.org/10.1139/tcsme-2020-0214.

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All-attitude flight simulators can simulate flight attitude through three rotational degrees of freedom. In this paper, the inverse kinematics and singularity of the all-attitude simulator are analyzed. Because a singularity will reduce the fidelity of the flight attitude simulation, we investigated ways to resolve this problem. An approximate method for quickly quantifying singularities is proposed. Static damping and dynamic damping are designed to optimize the singularity of the all-attitude simulator and improve the fidelity of flight attitude simulation. Attitude data of typical flight mo

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Gołębiewski, Michał, Marta Galant-Gołębiewska, and Remigiusz Jasiński. "Flight Simulator’s Energy Consumption Depending on the Conditions of the Air Operation." Energies 15, no. 2 (2022): 580. http://dx.doi.org/10.3390/en15020580.

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Protection of the natural environment is a key activity driving development in the transport discipline today. The use of simulators to train civil aviation pilots provides an excellent opportunity to maintain the balance between efficiency and limit the negative impact of transport on the environment. Therefore, we decided to determine the impact of selected simulations of air operations on energy consumption. The aim of the research was to determine the energy consumption of the flight simulator depending on the type of flight operation and configuration used. We also decided to compare the

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Дмитренко, Андрей Юрьевич. "FLIGHT SIMULATOR TRAINING AND ITS ROLE IN ENSURING FLIGHT SAFETY." ПРОБЛЕМЫ БЕЗОПАСНОСТИ ПОЛЕТОВ, no. 4 (July 1, 2024): 37–45. http://dx.doi.org/10.36535/0235-5000-2024-04-4.

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В статье излагаются ключевые аспекты, связанные с повышением безопасности полетов воздушных судов за счет широкого и целенаправленного применения авиационных тренажеров. Приводится классификация авиационных тренажеров и решаемые с их помощью задачи. Подчеркивается, что тренажерная подготовка, являясь этапом, предваряющим летную деятельность, решает задачу окончательного формирования готовности летчиков к выполнению полетов в нормальных условиях и при возникновении нештатных (аварийных) ситуаций, тем самым обеспечивая необходимый уровень безопасности полетов. The article outlines key aspects re

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Huiru, Li. "Design and Implementation of Mechanical Instrument for Flight Simulator." MATEC Web of Conferences 291 (2019): 01007. http://dx.doi.org/10.1051/matecconf/201929101007.

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The mechanical simulation instrument of flight simulator can meet the display visual error specified by the new regulations. By studying the working principle of the flight simulator mechanical simulation instrument, it can be seen that the mechanical simulation instrument can be quickly converted into other instruments of the same series by changing the dial. Taking the oxygen pressure indicating instrument of flight simulator as an example, this paper introduces the design principle, design circuit diagram, design angle calculation and software architecture of the instrument. It was installe

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Somerville, Alexander, Keith Joiner, and Graham Wild. "Effects of Flight Experience or Simulator Exposure on Simulator Sickness in Virtual Reality Flight Simulation." Multimodal Technologies and Interaction 9, no. 3 (2025): 24. https://doi.org/10.3390/mti9030024.

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The use of virtual reality (VR) for flight simulation, particularly in the earliest stages of pilot training, is gaining attention in both research and industry. The use of the technology for this ab initio training requires suitable consideration of the risks of simulator sickness—risks that are heightened relative to conventional simulators. If simulator sickness results in the development of compensatory skills, or otherwise disrupts the training process, the benefits of the technology may be negated. Enabling the effective integration of VR within flight training requires that, to the exte

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M., Zaouche* K. Foughali M. Amini and I. Boureghda. "DEVELOPMENT, INTEGRATION AND IMPLEMENTATION OF AN AIRCRAFT’S VIRTUAL MODEL IN MICROSOFT FLIGHT SIMULATOR." INTERNATIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH TECHNOLOGY 5, no. 8 (2016): 31–45. https://doi.org/10.5281/zenodo.59952.

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Commercialized flight simulators are considered as a training tool for aircrafts, validated by pilots of real systems. The aerodynamic aspect of aircrafts existing on the libraries of these simulators is treated in a shallow way. For example, the MicroSoft Flight Simulator 2004 (MSFS 2004), which is used in this work, uses the file “aircraft.cfg” of the folder “Flight Simulator 9” to stock some values that will be multiplied by the aerodynamic coefficients derivatives that are considered unknown and vary in time. These aerodynamic coefficients are important in the evalu

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Hong, Liu. "Electric Servo Loading System Applied to Flight Simulator." Applied Mechanics and Materials 380-384 (August 2013): 572–75. http://dx.doi.org/10.4028/www.scientific.net/amm.380-384.572.

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Flight simulator control loading system is an important part of the flight simulator, and it provides operating force people feeling system for Pilots. This paper introduces the working principle of digital control load system, and describes in detail the simulation and application of the electric servo loading system in the flight simulator. After tested the system has reached the ideal simulation results.

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Sultan, Cornel, Martin Corless, and Robert E. Skelton. "Tensegrity Flight Simulator." Journal of Guidance, Control, and Dynamics 23, no. 6 (2000): 1055–64. http://dx.doi.org/10.2514/2.4647.

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Qi, Pan Guo, D. C. Cong, H. J. Jiang, and Jun Wei Han. "Systems Analysis for Commercial Aircraft Flight Simulator." Applied Mechanics and Materials 10-12 (December 2007): 522–27. http://dx.doi.org/10.4028/www.scientific.net/amm.10-12.522.

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Flight simulator is a complex man-in-the-loop (MIL) simulation system. With several decades of development, it has already become important tools of aircraft design and development, and necessary means of pilot training. And simulation credibility and reliability of the flight simulator have been considerably improved in comparison with the past. However, the system of flight simulator has become increasingly complex and difficult to be described clearly. This paper presents the concepts of conceptual layer and achieving layer, analyzes the composition and principle of the commercial aircraft

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Wei, Ming-Yen, Shen-An Fang, and Ji-Wei Liu. "Design and Implementation of a New Training Flight Simulator System." Sensors 22, no. 20 (2022): 7933. http://dx.doi.org/10.3390/s22207933.

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Aircraft flight simulators have good cost efficiency, high reusability, and high flight safety. All airlines and aircraft manufacturing companies choose it as sophisticated training equipment for ground simulation, effectively reducing pilot training costs, ensuring personnel safety and aircraft wear and tear. The new simulator proposed in this paper combines a digital motion-cueing algorithm, flight software and motion platform to make pilots feel as if they are in the real world. By using EtherCAT technology to drive the motion-cueing platform, it can improve the data transmission speed of t

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Siqueira, Guilherme de Carvalho, Mauro Caetano, Daniel Amaral, and Jorge Henrique Bidinotto. "Component definition innovation plan as a tool to allow flight simulator training device roadmapping." Aviation 29, no. 1 (2025): 30–38. https://doi.org/10.3846/aviation.2025.23175.

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The use of flight simulators as a complement to pilot training offers significant advantages in reducing costs and risks associated with aircraft accidents, in addition to increasing safety and situational awareness during the practical phases of flight. However, the development of equipment to support pilot training has been carried out with an exclusive focus on this application, overlooking the exploration of alternative uses or new business opportunities that could diversify revenue streams and foster innovation. In this study, a method was developed to identify components that support the

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Shen, Dong Kai, Zheng Hua Liu, and Shi Zhang Liu. "Friction Compensation Based Acceleration Feedback Control for Flight Simulator." Advanced Materials Research 139-141 (October 2010): 1702–7. http://dx.doi.org/10.4028/www.scientific.net/amr.139-141.1702.

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The flight simulator is one kind of servo system with uncertainties and disturbances. To obtain high low-velocity performance and good robustness for the flight simulator, we present a novel robust controller based on the acceleration feedback and Disturbance Observer. Firstly, the plant model and the framework of the novel controller are described. Secondly, the principle and the design process of the acceleration feedback controller are analyzed and expatiated respectively. Finally, simulation results on the flight simulator show that the acceleration feedback controller can compensate nonli

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Kumar, Ashish, Sugjoon Yoon, and V. R. Sanal Kumar. "Mixed Reality Simulation of High-Endurance Unmanned Aerial Vehicle with Dual-Head Electromagnetic Propulsion Devices for Earth and Other Planetary Explorations." Applied Sciences 10, no. 11 (2020): 3736. http://dx.doi.org/10.3390/app10113736.

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One of the major limitations of existing unmanned aerial vehicles is limited flight endurance. In this study, we designed an innovative uninterrupted electromagnetic propulsion device for high-endurance missions of a quadcopter drone for the lucrative exploration of earth and other planets with atmospheres. As an airborne platform, this device could achieve scientific objectives better than state-of-the-art revolving spacecraft and walking robots, without any terrain limitation. We developed a mixed reality simulation based on a quadcopter drone and an X-Plane flight simulator. A computer with

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Allerton, D. J. "The case for flight simulation in general aviation." Aeronautical Journal 106, no. 1065 (2002): 607–12. http://dx.doi.org/10.1017/s0001924000018261.

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AbstractThis paper sets out the case to extend the role of flight simulation in general aviation. It outlines the benefits that flight simulation has brought to airline safety but observes that the majority of pilots worldwide receive no simulator-based training or checking. The paper reviews the potential benefits of synthetic training and provides an analysis of accidents in general aviation to show that a significant reduction in fatal accidents is achievable by instituting recurrent pilot checks in a flight simulator, similar to the simulator checks undertaken by airline pilots. The paper

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Allerton, D. J. "The case for flight simulation in general aviation." Aeronautical Journal 106, no. 1065 (2002): 607–12. http://dx.doi.org/10.1017/s0001924000011611.

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AbstractThis paper sets out the case to extend the role of flight simulation in general aviation. It outlines the benefits that flight simulation has brought to airline safety but observes that the majority of pilots worldwide receive no simulator-based training or checking. The paper reviews the potential benefits of synthetic training and provides an analysis of accidents in general aviation to show that a significant reduction in fatal accidents is achievable by instituting recurrent pilot checks in a flight simulator, similar to the simulator checks undertaken by airline pilots. The paper

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Aláez, Daniel, Xabier Olaz, Manuel Prieto, Pablo Porcellinis, and Jesús Villadangos. "HIL Flight Simulator for VTOL-UAV Pilot Training Using X-Plane." Information 13, no. 12 (2022): 585. http://dx.doi.org/10.3390/info13120585.

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With the increasing popularity of vertical take-off and landing unmanned aerial vehicles (VTOL UAVs), a new problem arises: pilot training. Most conventional pilot training simulators are designed for full-scale aircrafts, while most UAV simulators are just focused on conceptual testing and design validation. The X-Plane flight simulator was extended to include new functionalities such as complex wind dynamics, ground effect, and accurate real-time weather. A commercial HIL flight controller was coupled with a VTOL convertiplane UAV model to provide realistic flight control. A real flight case

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Zhang, Lei, H. Z. Jiang, and H. R. Li. "PC-Based Human-In-the-Loop Simulation for Flight." Applied Mechanics and Materials 10-12 (December 2007): 476–82. http://dx.doi.org/10.4028/www.scientific.net/amm.10-12.476.

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The development of a flight simulator is a challenging work because of its complexity and tremendous cost. We implement a prototype composed of PC cluster and have proved its coordination character as a flight training device. This paper describes the architecture of the flight simulator, the software development tools and hardware platform. These software and hardware constitute a PC based simulation environment and make the expense of the simulation application affordable. We also present the simulation modeling process. For the integrity of the cueing system, we designed a virtual prototype

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Wang, Tao, Ming Chao Zhu, Sheng Li Yin, and Hong Guang Jia. "Precision Analysis of Simulation Systems with Hardware-in-Loop Caused by Performance of Three-Axis Virtual Flight Motion Simulator." Advanced Materials Research 383-390 (November 2011): 4860–64. http://dx.doi.org/10.4028/www.scientific.net/amr.383-390.4860.

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Simulation systems with hardware-in-loop are composed by three-Axis virtual flight motion simulator, simulation computer, load torque simulator, and visual simulation systems. Three-Axis Virtual Flight Motion Simulator are used to simulate the attitude of missile in simulation system with hardware-in-loop, so its performance influenced the result of simulation directly. This paper mainly analyzed the factors which influenced the performance of a three-Axis virtual flight motion simulator which we are used now in the lab, then analyzed the entire simulation system’s error caused by these factor

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Liu, Xiao Feng, Jing Wei Yu, Hai Tao Wang, and Zhao Wen Fang. "Dynamic Analysis Helicopter Flight Simulator." Applied Mechanics and Materials 543-547 (March 2014): 1305–8. http://dx.doi.org/10.4028/www.scientific.net/amm.543-547.1305.

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For helicopter structural characteristics, this article focuses on the helicopter to take off, hover and other state aerodynamic analysis, the establishment of the fuselage-landing gear dynamics model; while the helicopter simulator simulation system are described, and the kinetic model was built simulation analysis, simulation results and the actual flight conditions consistent, indicating that the model is correct, there is a certain reference value.

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Savaş, Tamer, Uğur Özdemir, and Yunus Emre Esen. "The Role of Flight Simulators in Pilot Training." Journal of Aviation 9, no. 1 (2025): 137–45. https://doi.org/10.30518/jav.1588557.

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Aviation is one of the most advanced and multifaceted industries in the world. One of the most critical aspects of aviation, which cannot be overlooked, is flight safety. Pilot training is a specialized form of education that is a crucial component of the aviation industry. The training process serves as a fundamental interface between pilots and the potential environments they will encounter in real flight operations. At present, a significant portion of pilot training is performed in flight simulators, which replicate real flight environments, making pilot training both cost-effective and sa

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Li, Zhao Hui, and Gang Li. "Extending FMCS Test for Flight Simulation." Applied Mechanics and Materials 88-89 (August 2011): 72–76. http://dx.doi.org/10.4028/www.scientific.net/amm.88-89.72.

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By means of a simulator we could expand the test research scope which could not be reached with flight tests, and recover and repeat some special domain of the test course, and make many kinds of experiments about FMCS properties, functions and with embedded failures by combining simulation tests with practical structure. The reliability and creditability of simulation results could be increased under real FMCS in conjunction with semi-entity simulation. Simulators combining a real FMCS with digital simulation have been used extensively for evaluating the large matrix of FMCS contents.

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BALABAN, Anton, Andrei NEAMTU, Sorin BERBENTE, et al. "Considerations regarding the composition of the cockpit view for a modern simulator." INCAS BULLETIN 15, no. 2 (2023): 3–10. http://dx.doi.org/10.13111/2066-8201.2023.15.2.1.

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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) Sup

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Shen, Dong Kai, Jing Jing Wang, and Zheng Hua Liu. "Robust BackStepping Control Based DRNN for Flight Simulator." Advanced Materials Research 139-141 (October 2010): 1708–13. http://dx.doi.org/10.4028/www.scientific.net/amr.139-141.1708.

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Flight motion simulator is one kind of servo system with uncertainties and nonlinearities. To acquire higher frequency response and good robustness for the flight simulator, we present a Backstepping controller based on a Diagonal Recurrent Neural Network (DRNN) to work out this problem. For one thing, the design procedure of the robust Backstepping controller is described. Subsequently, the principle and the design steps of DRNN are analyzed and expatiated respectively. In the end, simulation results on the flight motion simulator show that robust backstepping control based on DRNN can compen

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Fowlkes, J. E., R. S. Kennedy, and M. G. Lilienthal. "Postural Disequilibrium following Training Flights." Proceedings of the Human Factors Society Annual Meeting 31, no. 5 (1987): 488–91. http://dx.doi.org/10.1177/154193128703100501.

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The use of flight simulators for training military aircrew and commercial pilots has been increasing dramatically since World War II. However, the advantages of simulator training, such as cost-effectiveness and variety of missions which can be safely flown, may be offset by the occurrence of ataxia and other symptoms associated with simulator training. The present paper reports on postural disequilibrium following training in eight Navy flight simulators. Tests of standing steadiness were administered to 726 Naval and Marine Corps aviators prior to and then just following their regular flight

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Dolzhenko, N., and E. Mailyanova. "Aviation simulator software, typical functions and its development prospects." Bulletin of the National Engineering Academy of the Republic of Kazakhstan 82, no. 4 (2021): 72–76. http://dx.doi.org/10.47533/2020.1606-146x.132.

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Flight simulators have been used for more than eighty years. The development of aircraft simulators that simulate the pilot’s work in the cockpit, the conditions of take-off, flight, landing, as well as the work of the dispatcher to train and maintain the professional level of aviation specialists is being addressed worldwide[1]. Training complexes can be divided into several parts, one of which is software. The instructor’s workstation software allows him to set various parameters of take-off, flight and landing conditions, as well as monitor and control the simulator subsystems. The article

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Jin, Rong. "Design of vehicular flight test simulation platform for a civil airplane." Journal of Physics: Conference Series 2336, no. 1 (2022): 012018. http://dx.doi.org/10.1088/1742-6596/2336/1/012018.

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Abstract During the flight test process of newly developed civil airplane, flight tests are often carried out at several typical airports according to different tasks such as high humidity, high temperature and low temperature tests. Using a vehicular flight test simulator to support flight test task not only can address the needs of multi-regional flight test tasks, but also can provide effective support for ensuring flight test safety and improving flight test efficiency. Aiming at the vehicular flight test simulation platform, an extendable vehicle platform is designed to make it has enough

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Pavel, M. D., M. White, G. D. Padfield, G. Roth, M. Hamers, and A. Taghizad. "Validation of mathematical models for helicopter flight simulators past, present and future challenges." Aeronautical Journal 117, no. 1190 (2013): 343–88. http://dx.doi.org/10.1017/s0001924000008058.

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Abstract At the heart of a flight simulator resides the mathematical representation of aircraft behaviour in response to control inputs, atmospheric disturbances and system inputs including failures and malfunctions. While this mathematical model can never be wholly accurate, its fidelity, in comparison with real world behaviour, underpins the usefulness of the flight simulator. The present paper examines the state of the art achieved in validating mathematical models for helicopter simulators, addressing the strengths and weaknesses of the present European standard for the qualification of he

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Pradhan, Gaurav N., Raquel C. Galvan-Garza, Alison M. Perez, Jan Stepanek, and Michael J. Cevette. "Visual Vestibular Conflict Mitigation in Virtual Reality Using Galvanic Vestibular Stimulation." Aerospace Medicine and Human Performance 93, no. 5 (2022): 406–14. http://dx.doi.org/10.3357/amhp.5921.2022.

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BACKGROUND: Virtual reality (VR) is an effective technique to reduce cost and increase fidelity in training programs. In VR, visual and vestibular cues are often in conflict, which may result in simulator-induced motion sickness. The purpose of this study is to investigate the integration of Galvanic Vestibular Stimulation (GVS) with a VR flight training simulator by assessing flight performance, secondary task performance, simulator sickness and presence.METHODS: There were 20 participants who performed 2 separate VR flight simulation sessions, with and without GVS (control). Flight performan

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Tong, Yu, Haoyun Zhou, Zhao Wu, Qifu Li, and Bei Lu. "Model Predictive Control Based Washout Algorithm Design for Flight Simulator Upset Prevention and Recovery Training." Aerospace 10, no. 10 (2023): 886. http://dx.doi.org/10.3390/aerospace10100886.

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To migrate Loss of Control In-flight, the number one cause of aviation fatalities, pilots need to undergo upset prevention and recovery training with flight simulators. The fidelity of a moving base flight simulator is greatly dependent on the washout algorithm of the Stewart platform, which may reach the workspace limits when simulating the aircraft recovery from upset conditions. In this paper, a washout algorithm optimal design method based on the model predictive control technique is proposed for flight simulator upset prevention and recovery training. The parameters of the washout algorit

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Deters, Robert W., Glen A. Dimock, and Michael S. Selig. "Icing Encounter Flight Simulator." Journal of Aircraft 43, no. 5 (2006): 1528–37. http://dx.doi.org/10.2514/1.20364.

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Siota, Toshiharu. "Visual simulations. Flight simulator." Journal of the Institute of Television Engineers of Japan 43, no. 1 (1989): 21–26. http://dx.doi.org/10.3169/itej1978.43.21.

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Kabanyachyi, Volodymyr, and Beycan Ibrahimoglu. "Consideration of the problem of motion cueing along angular degrees of freedom on flight simulators." Technology audit and production reserves 6, no. 1(74) (2023): 6–12. http://dx.doi.org/10.15587/2706-5448.2023.293498.

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The object of research is motion cueing along angular degrees of freedom on flight simulators of non-maneuvering aircraft. One of the most problematic places is lack of statement and effective solution of the problem to ensure high-quality motion cues along angular degrees of freedom on flight simulators, which would correspond to motion cues along angular degrees of freedom in real flight with the same control actions. In the course of the research, on the basis of the peculiarities of human movement perception, a set of characteristic attributes of perception of motion cues is determined: ch

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GĂINĂ, Laurențiu-Ioan, and Sorin PARASCHIV. "FLIGHT SIMULATOR TRAINING: PSYCHOPHYSIOLOGICAL RESPONSE." Review of the Air Force Academy 22, no. 1 (2024): 71–76. http://dx.doi.org/10.19062/1842-9238.2024.22.1.9.

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Flight simulators have become indispensable in the aviation industry, providing accurate and detailed simulations of cockpit and environmental conditions. They serve a variety of purposes, including pilot training, aircraft design, and accident investigation. While simulators are able to replicate many aspects of real-world flying, there are still differences in stress levels and response intensities. As such, a comprehensive training program that includes both simulated and real-world experiences is necessary to ensure pilots are well-prepared for handling the diverse challenges of aviation o

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Liu, Xiang Ming, and Xi Juan Hu. "Analysis and Research on Structural Dynamics of Three-Axis Flight Simulator." Applied Mechanics and Materials 65 (June 2011): 57–61. http://dx.doi.org/10.4028/www.scientific.net/amm.65.57.

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This paper mainly aims at analyzing and researching on the dynamic characteristics of the three-axis flight simulator based on O-U-T type, by using multi-physical field analysis ALGOR. The paper gives out the low-order natural frequencies of three-axis simulator and its corresponding vibration modes under real load, and also presents the dynamic characteristics of harmonic response, transient response and response spectrum analysis under the influences of constraint and excitation. From the simulation results, found structure design and material property greatly affect on the dynamic performan

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