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Статті в журналах з теми "Fly-by-wire primary flight control"
McLean, D. "Aircraft flight control systems." Aeronautical Journal 103, no. 1021 (March 1999): 159–66. http://dx.doi.org/10.1017/s0001924000064976.
Повний текст джерелаDi 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 (June 2012): 679–90. http://dx.doi.org/10.1177/0954410011413986.
Повний текст джерелаWang, Xiao-Hui, Wei-Qian Yu, Chen-Bo Gu, and Yi Jiang. "PFCS Four-redundant Sidestick Randomly Dynamically Grouping Vote Technology." Journal of Physics: Conference Series 2281, no. 1 (June 1, 2022): 012016. http://dx.doi.org/10.1088/1742-6596/2281/1/012016.
Повний текст джерелаPermenter, Kathryn E., and Clifford C. Baker. "Task-Operator Study for the Primary Flight Control Center of Tarawa Class (LHA) Ships." Proceedings of the Human Factors Society Annual Meeting 33, no. 16 (October 1989): 1119–23. http://dx.doi.org/10.1177/154193128903301618.
Повний текст джерелаMuthard, Emily K. "The Contaminating Influence of Display Size on Flight Control, Risk Assessment, and Route Selection." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 49, no. 1 (September 2005): 73–77. http://dx.doi.org/10.1177/154193120504900117.
Повний текст джерелаCrowder, R., and C. Maxwell. "Simulation of a prototype electrically powered integrated actuator for civil aircraft." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 211, no. 6 (June 1, 1997): 381–94. http://dx.doi.org/10.1243/0954410971532749.
Повний текст джерелаCollinson, R. P. G. "Fly-by-wire flight control." Computing & Control Engineering Journal 10, no. 4 (August 1, 1999): 141–52. http://dx.doi.org/10.1049/cce:19990403.
Повний текст джерелаKuenen, L. P. S., and P. J. Silk. "Sex-biased trap capture and odor-stimulated upwind flight in the field by Rhagoletis mendax (Diptera: Tephritidae)." Canadian Entomologist 133, no. 2 (April 2001): 293–95. http://dx.doi.org/10.4039/ent133293-2.
Повний текст джерелаNICOLIN, Ilie, and Bogdan Adrian NICOLIN. "The fly-by-wire system." INCAS BULLETIN 11, no. 4 (December 8, 2019): 217–22. http://dx.doi.org/10.13111/2066-8201.2019.11.4.19.
Повний текст джерелаCranshaw, Whitney, and Matthew Camper. "Management of Poplar Twiggall Fly on Nursery-grown Aspen." Journal of Environmental Horticulture 25, no. 1 (March 1, 2007): 33–35. http://dx.doi.org/10.24266/0738-2898-25.1.33.
Повний текст джерелаДисертації з теми "Fly-by-wire primary flight control"
MORNACCHI, ANDREA. "Design and development of prognostic and health management system for fly-by-wire primary flight control." Doctoral thesis, Politecnico di Torino, 2016. http://hdl.handle.net/11583/2651742.
Повний текст джерелаGENTILE, ROCCO. "Advanced Diagnostic for Fly-By-Wire Flight Control Systems." Doctoral thesis, Politecnico di Torino, 2021. http://hdl.handle.net/11583/2934682.
Повний текст джерелаGautrey, 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.
Повний текст джерелаEPSRC; Avro International Aerospace.
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.
Повний текст джерелаGriffin, Stuart James. "Helicopter control law design using eigenstructure assignment." Thesis, University of York, 1997. http://etheses.whiterose.ac.uk/21041/.
Повний текст джерелаField, Edmund J. "Flying qualities of transport aircraft : precognitive or compensatory?" Thesis, Cranfield University, 1995. http://dspace.lib.cranfield.ac.uk/handle/1826/10636.
Повний текст джерелаDel, 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.
Повний текст джерелаTitle from document title page. Document formatted into pages; contains ix, 185 p. : ill. Includes abstract. Includes bibliographical references (p. 87-91).
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.
Повний текст джерелаThesis (M.S)--Wichita State University, College of Engineering, Dept. of Aerospace Engineering
"July 2007."
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.
Повний текст джерелаVenter, Jeanne Marie. "Autonomous air-to-air refueling : a comparison of control strategies." Thesis, Stellenbosch : Stellenbosch University, 2012. http://hdl.handle.net/10019.1/20239.
Повний текст джерелаENGLISH 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 are based on a mathematical aircraft model which was derived from a simulation model received from Airbus. The first set of controllers uses the aircraft actuators directly. Controllers that are based on the CG dynamics and the receptacle dynamics are compared. Due to the large distance between the CG and the receptacle it was found to be essential to control the receptacle position, and not only the CG position. Also, a controller that is based on a model of the receptacle dynamics performs better. The second set of controllers uses the aircraft manual control laws as an inner loop controller. This set of controllers and the last direct actuator controller use the same axial controller that uses the engine thrust to control axial position. It was found that both the direct actuator controller and the manual control laws controller are able to keep the receptacle within the disconnect envelope in moderate turbulence. In both sets of controllers the axial controller fails to keep the receptacle reliably within the disconnect envelope in light turbulence. From the results it is concluded that both the direct actuator control and manual control laws can be used to successfully control the receptacle position in the normal and lateral positions as long as the receptacle kinematics are included in the control design. Using only the engine thrust for axial control is insufficient. Several recommendations are made to improve the axial control and also how these results can be used in future work.
AFRIKAANSE OPSOMMING: Die lug-tot-lug brandstof hervulling van groot vliegtuie het uitdagings soos ’n lang hervullingstyd, stadige vliegtuig dinamika en ’n groot afstand tussen die hervullingspoort en die vliegtuig massamiddelpunt. Hierdie projek spreek sommige van hierdie uitdagings aan deur ’n beheerstelsel by te voeg wat die vliegtuig in die korrekte posisie relatief tot die tenker hou vir brandstofoordrag om plaas te vind. Hierdie projek ondersoek verskillende beheerstrategieë wat ontwerp is om die A330- 300 te beheer by ’n enkele gestadigde toestand. Die beheerders is gebaseer op ’n wiskundige vliegtuigmodel wat vanaf ’n simulasiemodel afgelei is. Die simulasiemodel is vanaf Airbus verkry. Die eerste stel beheerders beheer direk die vliegtuig se beheeroppervlakke. Beheerders wat onderskeidelik die massamiddelpunt en die hervullingspoort beheer word vergelyk. Daar is gevind dat dit essensieel is om die hervullingspoort te beheer en nie slegs die massamiddelpunt nie, as gevolg van die groot afstand tussen hierdie twee punte. Die tweede stel beheerders gebruik die vliegtuig se eie beheerwette as ’n binnelusbeheerder en vorm self die buitelus. Albei stelle beheerders gebruik dieselfde aksiale beheerder wat enjin stukrag gebruik om die aksiale posisie te beheer. Daar is gevind dat beide stelle beheerders die hervullingspoort binne die ontkoppelingsbestek kan hou in die normale en laterale rigtings tydens matige turbulensie. In beide stelle beheerders is dit die aksiale beheerder wat faal om die hervullingspoort betroubaar in posisie te hou, selfs in ligte turbulensie. Vanaf die resultate word afgelei dat beide die direkte beheerder en die buitelusbeheerder gepas is om die laterale en normale posisiebeheer toe te pas mits die dinamika van die hervullingspoort in ag geneem word. Om slegs stukrag te gebruik vir aksiale beheer is nie voldoende nie, en verskeie voorstelle word gemaak om die aksiale beheer te verbeter in toekomstige navorsing.
Книги з теми "Fly-by-wire primary flight control"
Dian chuan fei xing kong zhi xi tong: Fly-by-wire flight control system. Beijing: Guo fang gong ye chu ban she, 2003.
Знайти повний текст джерелаGautrey, J. Flight control system architecture analysis and design for a fly-by-wire generic regional aircraft. Cranfield, Bedford, England: Cranfield University, College of Aeronautics, 1996.
Знайти повний текст джерелаDroste, Carl S. A case study on the F-16 fly-by-wire flight control system. New York]: American Institute of Aeronautics and Astronautics, 1985.
Знайти повний текст джерелаF, Wanamaker Michael, and United States. National Aeronautics and Space Administration., eds. Optical closed-loop flight control demonstration: Fly-by-Light Aircraft Closed Loop Test (FACT) Program and Fly-by-Light Installation and Test (FIT) Program : under contract NAS3-25965. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаF, Wanamaker Michael, and United States. National Aeronautics and Space Administration., eds. Optical closed-loop flight control demonstration: Fly-by-Light Aircraft Closed Loop Test (FACT) Program and Fly-by-Light Installation and Test (FIT) Program : under contract NAS3-25965. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаF, Wanamaker Michael, and United States. National Aeronautics and Space Administration., eds. Optical closed-loop flight control demonstration: Fly-by-Light Aircraft Closed Loop Test (FACT) Program and Fly-by-Light Installation and Test (FIT) Program : under contract NAS3-25965. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаGibson, J. C. Development of a methodology for excellence in handling qualities design for fly by wire aircraft. Delft, Netherlands: Delft University Press, 1999.
Знайти повний текст джерелаTomayko, J. E. Computers take flight: A history of NASA's pioneering digital fly-by-wire project. Washington, D.C: NASA, 2000.
Знайти повний текст джерелаSundberg, Gale R. Civil air transport: A fresh look at power-by-wire and fly-by-light. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаFault tolerant flight control: A benchmark challenge. Berlin: Springer, 2010.
Знайти повний текст джерелаЧастини книг з теми "Fly-by-wire primary flight control"
Collinson, R. P. G. "Fly-by-wire flight control." In Introduction to Avionics, 119–76. Dordrecht: Springer Netherlands, 1996. http://dx.doi.org/10.1007/978-94-011-0007-6_4.
Повний текст джерелаCollinson, R. P. G. "Fly-by-Wire Flight Control." In Introduction to Avionics Systems, 179–253. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-94-007-0708-5_4.
Повний текст джерелаCollinson, R. P. G. "Fly-by-Wire Flight Control." In Introduction to Avionics Systems, 159–224. Boston, MA: Springer US, 2003. http://dx.doi.org/10.1007/978-1-4419-7466-2_4.
Повний текст джерелаLuo, Xin. "Research on Control Characteristics of Civil Aircraft Module Integration Fly by Wire Flight Control System." In Lecture Notes in Electrical Engineering, 345–54. Singapore: Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-6613-2_35.
Повний текст джерелаFavre, C. "Fly-by-wire for commercial aircraft: the Airbus experience." In Advances in Aircraft Flight Control, 211–29. Routledge, 2018. http://dx.doi.org/10.1201/9781315136820-8.
Повний текст джерелаNae, Cătălin, Ilie Nicolin, and Bogdan Adrian Nicolin. "Military Aircraft Flight Control." In Aeronautics - New Advances [Working Title]. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.105491.
Повний текст джерелаТези доповідей конференцій з теми "Fly-by-wire primary flight control"
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.
Повний текст джерелаMa, Carlton Y. "Fly-By-Wire Dual-Dual Flight Control Actuation System." In Aerospace Power Systems Conference. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1998. http://dx.doi.org/10.4271/981252.
Повний текст джерелаLyle, B. S. "Reducing Complexity in Fly-By-Wire Flight Control Actuators." In A-6 Symposium Program Advanced Actuation, Controls, and Integration for Aerospace Vehicles. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1985. http://dx.doi.org/10.4271/851752.
Повний текст джерелаWALTER, CHRIS. "MAFT - An architecture for reliable fly-by-wire flight control." In Digital Avionics Systems Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-3902.
Повний текст джерелаVIETEN, K. "High-performance fighter fly-by-wire flight control actuation system." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1123.
Повний текст джерелаTameh, 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.
Повний текст джерелаXue, Ying, Zhenqiang Yao, and Wei Niu. "The Distributed Dissimilar Redundancy Architecture of Fly-by-Wire Flight Control System." In 2016 12th International Conference on Computational Intelligence and Security (CIS). IEEE, 2016. http://dx.doi.org/10.1109/cis.2016.0072.
Повний текст джерелаShetty, Devdas, and Louis Manzione. "Unmanned Aerial Vehicles (UAV): Design Trends." In ASME 2011 International Mechanical Engineering Congress and Exposition. ASMEDC, 2011. http://dx.doi.org/10.1115/imece2011-64518.
Повний текст джерелаBerger, 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. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-0019.
Повний текст джерелаAlvarez, 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. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-4508.
Повний текст джерела