Relevant bibliographies by topics / Fly-by-Wire flight controls

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

Academic literature on the topic 'Fly-by-Wire flight controls'

Author: Grafiati
Published: 4 June 2021
Last updated: 12 February 2022

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Journal articles on the topic "Fly-by-Wire flight controls"

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Mulder, M., A. R. Veldhuijzen, M. M. van Paassen, and J. A. Mulder. "Integrating Fly-by-Wire Controls with Perspective Flight-Path Displays." Journal of Guidance, Control, and Dynamics 28, no. 6 (2005): 1263–74. http://dx.doi.org/10.2514/1.12617.

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McLean, D. "Aircraft flight control systems." Aeronautical Journal 103, no. 1021 (1999): 159–66. http://dx.doi.org/10.1017/s0001924000064976.

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Abstract This paper presents a short account of the flight control systems used in commercial transport, military combat and general aviation aircraft. The effects of aircraft safety, reliability and weather delays on satisfactory aircraft operations are shown to be significant reasons for the extensive use of flight control systems. The principles of flight control, the sensors and actuators required and the various modes which can be selected are treated, together with a short account of the primary flying controls and the use of manual reversion in emergency situations. The paper concludes
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Di Rito, G., and R. Galatolo. "Experimental assessment of the dynamic stiffness of a fault-tolerant fly-by-wire hydraulic actuator." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 226, no. 6 (2012): 679–90. http://dx.doi.org/10.1177/0954410011413986.

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The stiffness of an actuator depends on the closed-loop position control (architecture and parameters), on the load frequency, and, for fault-tolerant actuators, on the operative mode. The stiffness response is of basic importance for the design of actuators for primary flight controls, especially for high-performance aircrafts. Actually, during flight conditions characterized by high speed and high angle-of-attack, the dynamic interactions between aircraft structure, actuator, and aerodynamic loads can induce aeroservoelastic effects, which, if not controlled, can imply performance degradatio
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Rzucidło, Paweł. "MONITORING AND DATA ACQUISITION SYSTEM FOR EXPERIMENTAL GENERAL AVIATION FLY‐BY‐WIRE AIRCRAFT." Aviation 10, no. 3 (2006): 16–20. http://dx.doi.org/10.3846/16487788.2006.9635935.

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A CAN data bus was used in a project of an experimental Fly‐by‐Wire control system (SPS‐1) mounted on board a PZL‐110 “Koliber” general aviation aircraft. This solution allows the free communication between flight control computers and individual modules of the system. The monitoring of the bus state and data frames is useful during particular hardware tests, system integration, laboratory and in‐flight tests. This report intends to present the specific monitor tool developed with the to SPS‐1. The main part of the CAN monitoring system is software. It realizes acquisition, visualization and c
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Wright, W. E., and J. C. Hall. "Advanced Aircraft Gas Turbine Engine Controls." Journal of Engineering for Gas Turbines and Power 112, no. 4 (1990): 561–64. http://dx.doi.org/10.1115/1.2906205.

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With the advent of vectored thrust, vertical lift, and fly-by-wire aircraft, the complexity of aircraft gas turbine control systems has evolved to the point wherein they must approach or equal the reliability of current quad redundant flight control systems. To advance the technology of high-reliability engine controls, one solution to the Byzantine General’s problem (Lamport et al., 1982) is presented as the foundation for fault tolerant engine control architecture. In addition to creating a control architecture, an approach to managing the architecture’s redundancy is addressed.
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Lee, R. N. "Development of Active Control Technology for the Next Generation of Combat Aircraft." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 206, no. 1 (1992): 15–25. http://dx.doi.org/10.1243/pime_proc_1992_206_235_02.

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In the mid 1970s British Aerospace recognized that active control technology offered considerable benefits in terms of improved performance and combat effectiveness for future combat aircraft. However, the introduction of such technology carried with it a significant development risk. In order to minimize that risk, a series of flight demonstrator programmes were initiated. This paper describes the principles of active control and the very successful fly-by-wire Jaguar and experimental aircraft demonstrator flight test programmes which progressively demonstrated the viability and benefits of a
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Rogalski, Tomasz. "THE IDEA OF A SYSTEM INCREASING FLIGHT SAFETY." Aviation 14, no. 4 (2010): 112–16. http://dx.doi.org/10.3846/aviation.2010.17.

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This paper presents a conception of an airborne control system that can increase the safety of a general aviation aircraft. Sample threats appear on board the general aviation airplane discussed in the paper. The system monitors some events and flight parameters in the cockpit and can take some actions protecting the plane against threats if recognised as necessary. The paper presents sample actions fly‐by‐wire control systems can take to protect a plane against some threats on board. The system can modify a pilot's controls to correct flight and if it is not enough the system can disengage th
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Kruk, R. V., D. W. Runnings, M. King, A. L. Lippay, and G. M. McKinnon. "Development and Evaluation of a Proportional Displacement Sidearm Controller for Helicopters." Proceedings of the Human Factors Society Annual Meeting 30, no. 9 (1986): 865–69. http://dx.doi.org/10.1177/154193128603000903.

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Associated with the development of fly-by-wire control systems for use in helicopters has been the prospect of replacing all of the current manual flight controls in the cockpit with a single sidearm controller. For the most part, the technology available for this concept has consisted of variations of force sensing sidearm controllers. The human proprioceptive system, however, does not perform optimally in force discrimination and stable maintenance of force outputs. One consequence of this is that operator feedback with respect to direction and magnitude of control input with force sensing m
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Collinson, R. P. G. "Fly-by-wire flight control." Computing & Control Engineering Journal 10, no. 4 (1999): 141–52. http://dx.doi.org/10.1049/cce:19990403.

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Reichel, Reinhard. "Steuersysteme im Flugzeug – Fly-By-Wire (Flight Control Systems – Fly-By-Wire)." at - Automatisierungstechnik 52, no. 12-2004 (2004): 588–95. http://dx.doi.org/10.1524/auto.52.12.588.53458.

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Dissertations / Theses on the topic "Fly-by-Wire flight controls"

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Coïc, Clément. "MODEL-AIDED DESIGN OF A HIGH-PERFORMANCE FLY-BY-WIRE ACTUATOR, BASED ON A GLOBAL MODELLING OF THE ACTUATION SYSTEM USING BOND-GRAPHS." Thesis, Toulouse, INSA, 2016. http://www.theses.fr/2016ISAT0042.

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Afin d’introduire de nouvelles fonctions dans les commandes de vol d’hélicoptère, il est nécessaire d’augmenter les bandes passantes de leurs actionneurs. La modélisation réaliste de l’ensemble du système d’actionnement, rendant compte de ses limitations de puissance et de sa consommation énergétique, ainsi que l’amélioration des technologies existantes des dispositifs d’étanchéité et de guidage sont les deux enjeux principaux permettant d’atteindre la durée de vie souhaitée à hautes fréquences. Pour supporter ce nouveau développement, ce travail s’organise en trois parties. Une première parti
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Gautrey, Jim. "Flying qualities and flight control system design for a fly-by-wire transport aircraft." Thesis, Cranfield University, 1998. http://dspace.lib.cranfield.ac.uk/handle/1826/9594.

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Fly-by-wire flight control systems are becoming more common in both civil and military aircraft. These systems give many benefits, but also present a new set of problems due to their increased complexity compared to conventional systems and the larger choice of options that they provide. The work presented here considers the application of fly-by-wire to a generic regional transport aircraft. The flying qualities criteria used for typical flying qualities evaluations are described briefly followed by analysis of several past transport aircraft flying qualities programmes against these criteria
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Cochoy, Olaf. "Investigations for the synchronized operation of a hybrid actuator configuration in redundant flight control systems." Aachen Shaker, 2009. http://d-nb.info/999024698/04.

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Field, Edmund J. "Flying qualities of transport aircraft : precognitive or compensatory?" Thesis, Cranfield University, 1995. http://dspace.lib.cranfield.ac.uk/handle/1826/10636.

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The introduction of fly-by-wire electronic flight control systems into transport aircraft has given the flying qualities engineer the opportunity to optimise the flying qualities of these aircraft for their specific tasks. With this technology has come the opportunity to introduce new technologies into the cockpit, such as non-linked or backfed sidesticks and non-backfed throttle levers. A comparative survey of airline pilots flying such a very high technology unconventional aircraft and a high technology but conventional aircraft suggests that these technologies may reduce the available chann
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Griffin, Stuart James. "Helicopter control law design using eigenstructure assignment." Thesis, University of York, 1997. http://etheses.whiterose.ac.uk/21041/.

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Del, Gobbo Diego. "Formal specification of requirements for analytical redundancy based fault tolerant flight control systems." Morgantown, W. Va. : [West Virginia University Libraries], 2000. http://etd.wvu.edu/templates/showETD.cfm?recnum=1629.

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Thesis (Ph. D.)--West Virginia University, 2000.<br>Title from document title page. Document formatted into pages; contains ix, 185 p. : ill. Includes abstract. Includes bibliographical references (p. 87-91).
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Chandramohan, Rajeev. "Adaptive critic flight control for a general aviation aircraft: Simulations for the beech bonanza fly-by-wire testbed." Thesis, Wichita State University, 2007. http://hdl.handle.net/10057/1509.

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An adaptive and reconfigurable flight control system is developed for a general aviation aircraft. The flight control system consisting of two neural networks is developed using a two phase procedure called the pre-training phase and the online training phase. The adaptive critic method used in this thesis was developed by Ferrari and Stengel. In the pre-training phase the architecture and initial weights of the neural network are determined based on linear control. A set of local gains for the linearized model of the plant is obtained at different design points on the velocity v/s altitude en
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Chandramohan, Rajeev Steck James E. "Adaptive critic flight control for a general aviation aircraft: Simulations for the beech bonanza fly-by-wire testbed /." Thesis, A link to full text of this thesis in SOAR, 2007. http://hdl.handle.net/10057/1509.

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Venter, Jeanne Marie. "Autonomous air-to-air refueling : a comparison of control strategies." Thesis, Stellenbosch : Stellenbosch University, 2012. http://hdl.handle.net/10019.1/20239.

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Thesis (MScEng)--Stellenbosch University, 2012.<br>ENGLISH ABSTRACT: The air-to-air refuelling of large aircraft presents challenges such as a long fuel transfer time, slow aircraft responses and a large distance between the aircraft CG and the receptacle position. This project addresses some of these issues by adding a control system to keep the receiver aircraft in the correct position relative to the tanker to enable fuel transfer. This project investigates different control strategies which are designed to control the A330-300 during refuelling at one trim condition. The controllers
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Books on the topic "Fly-by-Wire flight controls"

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Dian chuan fei xing kong zhi xi tong: Fly-by-wire flight control system. Guo fang gong ye chu ban she, 2003.

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Droste, Carl S. A case study on the F-16 fly-by-wire flight control system. American Institute of Aeronautics and Astronautics, 1985.

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Gautrey, J. Flight control system architecture analysis and design for a fly-by-wire generic regional aircraft. Cranfield University, College of Aeronautics, 1996.

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Fault tolerant flight control: A benchmark challenge. Springer, 2010.

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Gibson, J. C. Development of a methodology for excellence in handling qualities design for fly by wire aircraft. Delft University Press, 1999.

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Tomayko, J. E. Computers take flight: A history of NASA's pioneering digital fly-by-wire project. NASA, 2000.

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Tomayko, J. E. The story of self-repairing flight control systems. NASA Dryden Flight Research Center, 2003.

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Sundberg, Gale R. Civil air transport: A fresh look at power-by-wire and fly-by-light. NASA, 1990.

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Hamel, Peter. Fliegende Simulatoren und Technologieträger: Braunschweiger Luftfahrtforschung im internationalen Umfeld. Appelhans Verlag, 2014.

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Langewiesche, William. Fly by wire: The geese, the glide, the Miracle on the Hudson. Thorndike Press, 2009.

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Book chapters on the topic "Fly-by-Wire flight controls"

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Collinson, R. P. G. "Fly-by-Wire Flight Control." In Introduction to Avionics Systems. Springer US, 2003. http://dx.doi.org/10.1007/978-1-4419-7466-2_4.

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Collinson, R. P. G. "Fly-by-wire flight control." In Introduction to Avionics. Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_4.

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Collinson, R. P. G. "Fly-by-Wire Flight Control." In Introduction to Avionics Systems. Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-0708-5_4.

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de Montalk, Peter Potocki, and Gregg Bartley. "Fly-By-Wire Flight Controls." In Digital Avionics Handbook, Second Edition - 2 Volume Set. CRC Press, 2000. http://dx.doi.org/10.1201/9781420036879.sec2.

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Bartley, Gregg F. "Boeing B-777: Fly-by-Wire Flight Controls." In Digital Avionics Handbook. CRC Press, 2017. http://dx.doi.org/10.1201/b17545-29.

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"Boeing B-777: Fly-by-Wire Flight Controls." In Digital Avionics Handbook. CRC Press, 2000. http://dx.doi.org/10.1201/9781420036879-17.

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"Boeing B-777: Fly-By-Wire Flight Controls." In Avionics. CRC Press, 2018. http://dx.doi.org/10.1201/9781315222240-32.

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Favre, C. "Fly-by-wire for commercial aircraft: the Airbus experience." In Advances in Aircraft Flight Control. Routledge, 2018. http://dx.doi.org/10.1201/9781315136820-8.

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Conference papers on the topic "Fly-by-Wire flight controls"

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Lyle, B. S. "Reducing Complexity in Fly-By-Wire Flight Control Actuators." In A-6 Symposium Program Advanced Actuation, Controls, and Integration for Aerospace Vehicles. SAE International, 1985. http://dx.doi.org/10.4271/851752.

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Zaal, Peter, Daan Pool, Alexander in 't Veld, et al. "Design and Certification of a Fly-by-Wire System with Minimal Impact on the Original Flight Controls." In AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-5985.

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Ferrara, Davide, Giovanni Jacazio, Andrea Mornacchi, and Massimo Sorli. "Robust Mechatronic Actuation System for UAV Primary Flight Controls." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-85339.

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The paper describes the initial results of a research activity aimed at developing a high integrity mechatronic system for UAVs primary flight controls able to ensure the necessary flight safety and to enhance the system availability by implementing appropriate prognostic functions. In this system a flight control surface is driven by two parallel rollerscrews, on their turn driven by brushless motors equipped with gearhead and clutch; the motors electric drives are controlled by dual redundant electronic units performing closed loop position control as a function of the commands received from
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Ma, Carlton Y. "Fly-By-Wire Dual-Dual Flight Control Actuation System." In Aerospace Power Systems Conference. SAE International, 1998. http://dx.doi.org/10.4271/981252.

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WALTER, CHRIS. "MAFT - An architecture for reliable fly-by-wire flight control." In Digital Avionics Systems Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3902.

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VIETEN, K. "High-performance fighter fly-by-wire flight control actuation system." In Aerospace Design Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1123.

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Tameh, Tahereh Ahmadi, Mohamad Sawan, and Raman Kashyap. "Fly-by-wire flight control smart optical rotary sensor for aircraft." In 2016 Photonics North (PN). IEEE, 2016. http://dx.doi.org/10.1109/pn.2016.7537895.

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Berger, Tom, Mark Tischler, and Steven G. Hagerott. "Piloted Simulation Handling Qualities Assessment of a Business Jet Fly-By-Wire Flight Control System." In AIAA Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-0019.

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Alvarez, Daniel J., David H. Klyde, Marco Lotterio, and Tony Lambregts. "Fixed-Base Piloted Simulation Evaluation of Pitch Axis Fly-By-Wire Flight Control System Characteristics." In AIAA Atmospheric Flight Mechanics (AFM) Conference. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-4508.

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BAILEY, RANDALL. "The application of pilot rating and evaluation data for fly-by-wire flight control system design." In 17th Atmospheric Flight Mechanics Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-2826.

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