Relevant bibliographies by topics / Flight management system

Contents

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

Academic literature on the topic 'Flight management system'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Flight management system"

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Pressdee, AW. "Flight Management System." Aircraft Engineering and Aerospace Technology 59, no. 6 (June 1987): 4–5. http://dx.doi.org/10.1108/eb036455.

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Patrón, R. S. Félix, A. Kessaci, and R. M. Botez. "Horizontal flight trajectories optimisation for commercial aircraft through a flight management system." Aeronautical Journal 118, no. 1210 (December 2014): 1499–518. http://dx.doi.org/10.1017/s0001924000010162.

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Abstract To reduce aircraft emissions to the atmosphere, the fuel burn from aircraft has to be reduced. For long flights, the cruise is the phase where the most significant reduction can be obtained. A new horizontal profile optimisation methodology to achieve lower emissions is described in this article. The impact of wind during a flight can reduce the flight time, either by taking advantage of tailwinds or by avoiding headwinds. A set of alternative trajectories are evaluated to determine the quickest flight time, and therefore, the lowest fuel burn. To determine the expected amount of fuel reduction, the performance databases used on actual FMS devices, were used. These databases represent the flight performance of commercial aircraft.
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Faerber, Bob. "Advanced flight management system human interface." Air & Space Europe 1, no. 1 (January 1999): 42–44. http://dx.doi.org/10.1016/s1290-0958(99)80036-7.

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Abdi, M. Reza, and Sanjay Sharma. "Information system for flight disruption management." International Journal of Information Management 28, no. 2 (April 2008): 136–44. http://dx.doi.org/10.1016/j.ijinfomgt.2008.01.006.

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Fiyanzar, Adin Eka, Dewi Nusraningrum, and Osman Arofat. "PENERAPAN SAFETY MANAGEMENT SYSTEM PADA LEMBAGA PENYELENGGARA PELAYANAN NAVIGASI PENERBANGAN INDONESIA." JURNAL MANAJEMEN TRANSPORTASI DAN LOGISTIK 3, no. 2 (July 11, 2017): 205. http://dx.doi.org/10.25292/j.mtl.v3i2.95.

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This study aimed to analyze the effect of the implementation of Safety Management System (SMS) and the use of information system on the Flight Safety in the Indonesian Air Navigation Services Organization both partially and simultaneously. The research uses quantitative methods, and the data are analyzed using linear regression, simple correlation both partially and simultaneously and path analysis. The result shows; implementation of Safety Management System (X1) as measured by the Flight Safety (Y) has a positive and significant contribution on the level of Flight Safety. The amount of the application contribution of Safety Management System that directly contributes to the Flight Safety is 35.4%, so the research hypothesis which states that the Safety Management System application directly impacts significantly on Aviation Safety is accepted; the use of Information Systems (X2) as measured by the Flight Safety (Y) has a positive and significant contribution on the level of Flight Safety. The use of information systems contributions that directly contributes to aviation safety is 38.4%, so the hypothesis which states that the use of information system directly affects significantly the flight safety is acceptable; the total effect of simultaneous application of Safety Management System (X1) and the use of Information Systems (X2) contribute significantly to the Flight Safety (Y) as much as 66.3%. The remaining 33.7% is the influence of the other factors such as refresher and development training for air navigation personnel, aviation navigation equipment renewal and observation flight
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Hegyi, Norbert, and János Jósvai. "Unmanned Free Balloon Flight’s Integration into Unmanned Aircraft System Traffic Management." Acta Technica Jaurinensis 12, no. 4 (October 29, 2019): 321–34. http://dx.doi.org/10.14513/actatechjaur.v12.n4.522.

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This paper describes and inspects unmanned aerial vehicle, unmanned aircraft system, unmanned aircraft system traffic management, light and medium unmanned free balloons. It presents future safety developments and goals of the European Union’s own airspace, but also the Hungarian free route airspace. The development and realization of Swiss U-Space is discussed. Hungarian flights statistics are analyzed. Based on statistics, realized and under development solutions there are recommendations in the paper for the integration of the flight tacking for the mentioned balloons. A real flight tracking test has been done and it is shown in this paper. Its properties are analyzed with conclusions for possible usage.
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Combs, S. R., R. C. Loschke, and G. J. Tauke. "Flight management system of the F-117A." IEEE Aerospace and Electronic Systems Magazine 7, no. 7 (July 1992): 49–55. http://dx.doi.org/10.1109/62.149796.

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Bosch, D., M. A. Rodríguez, and J. Avilla. "Captures of MFO-resistant Cydia pomonella adults as affected by lure, crop management system and flight." Bulletin of Entomological Research 106, no. 1 (October 26, 2015): 54–62. http://dx.doi.org/10.1017/s0007485315000772.

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AbstractThe main resistance mechanism of codling moth (Cydia pomonella) in the tree fruit area of Lleida (NE Spain) is multifunction oxidases (MFO). We studied the frequency of MFO-resistant adults captured by different lures, with and without pear ester, and flights in orchards under different crop management systems. The factor year affected codling moth MFO-resistance level, particularly in the untreated orchards, highlighting the great influence of codling moth migration on the spread of resistance in field populations. Chemical treatments and adult flight were also very important but mating disruption technique showed no influence. The second adult flight showed the highest frequency, followed by the first flight and the third flight. In untreated orchards, there were no significant differences in the frequency of MFO-resistant individuals attracted by Combo and BioLure. Red septa lures baited with pear ester (DA) captured sufficient insects only in the first generation of 2010, obtaining a significantly lower proportion of MFO-resistant adults than Combo and BioLure. In the chemically treated orchards, in 2009 BioLure caught a significantly lower proportion of MFO-resistant adults than Combo during the first and third flight, and also than DA during the first flight. No significant differences were found between the lures or flights in 2010. These results cannot support the idea of a higher attractiveness of the pear ester for MFO-resistant adults in the field but do suggest a high influence of the response to the attractant depending on the management of the orchard, particularly with regard to the use of chemical insecticides.
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Nikiforov, O. V., O. G. Dodonov, and V. G. Putyatin. "The use of information technologies in risk management for the flight safety of aviation." Mathematical machines and systems 1 (2021): 32–41. http://dx.doi.org/10.34121/1028-9763-2021-1-32-41.

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At present, the problem of ensuring the necessary level of state aviation flights safety in terms of hu-man and organizational factors is very urgent. Despite the ongoing measures aimed at expanding and strengthening control over the processes of aviation activity, flight incidents caused by insufficient reli-ability of personnel work and organizational errors continue to occupy leading positions. There is an in-sufficient efficiency of the flight safety management system to identify hazardous factors in their latent stage, which is necessary for the early prevention of accidents. The difficulty of timely identification of the aviation system dangerous states associated with these factors is due to the need to account, corre-late and analyze data of a very large dimension and multifacetedness. According to the authors, a suc-cessful solution to this problem is possible through the use of automated processing and cognitive com-bination of large heterogeneous information arrays based on centralized electronic systems for collect-ing, information and analytical processing and storage of information about the functioning of the avia-tion system, identified abnormal and dangerous conditions, and incidents that have already occurred. The article presents the concept of creating a promising automated flight safety management system for state aviation. The proposed system will make it possible to implement the principle of proactive detec-tion and prevention of hazardous factors and risks for flight safety, taking into account human and or-ganizational factors, based on the implementation of processes for centralized collection, generalization and analysis of big data on the state of the aviation system. Topical scientific tasks for the creation of a methodological basis for the development of special software for such an automated system have been formulated.
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Bachkalo, B. I., and V. I. Zolotykh. "Methodical apparatus for evaluating the state of aviation system safety and security." Civil Aviation High Technologies 22, no. 6 (December 26, 2019): 17–28. http://dx.doi.org/10.26467/2079-0619-2019-22-6-17-28.

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The article analyzes the existing problems that impede the effective safety management of the flights of the air forces of the Armed Forces of the Russian Federation. As a result, this analysis revealed the contradiction between the need to build a safety management system and the lack of effective mechanisms for assessing the state of the aviation system and taking into account the influence of the human factor of aviation professionals on flight safety. The contradiction identified the need for developing a set of methods to estimate the actual state of the aviation system protection from the effects of threats associated with the human factor of flight personnel. A methodological apparatus was developed for assessing the security status of an aviation system against hazardous factors, which is based on applying a personality-oriented approach to assessing and managing the state of an aviation system. The method of assessing the state of flight safety allows you to quantify the state of protection of the crew-aircraft system from the impact of hazards caused by the personal factor of a particular pilot before the flight and to assess in near real-time the state of protection of the crew-aircraft system during the flight. The method of assessing the state of safety in aviation formation allows you to assess the status of safety during the organization and conduct of flights, taking into account the influence of the human factor of flight personnel in near real time.
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Dissertations / Theses on the topic "Flight management system"

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Franěk, Lukáš. "Flight Management System Model." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2011. http://www.nusl.cz/ntk/nusl-219075.

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Diplomová práce shrnuje nejdůležitější informace o letectví, jako například základní používané termíny, popis letových fází apod. V této práci je popsán flight management system, jeho funkce a schopnosti vytvořit cenově příznivý a současně absolutně spolehlivý letový plán. V další části práce je nastíněna důležitost předpovědi počasí pro bezpečnou a současně cenově příznivou leteckou dopravu. Tato práce je vytvořena v programu Matlab a všechny bloky jsou naprogramovány jako m-funkce. Důležité části kódu jsou z důvodu názornosti zobrazeny jako vývojové diagramy. Praktická část práce je rozdělena do několika podkapitol, kde každá podkapitola popisuje jeden blok z blokového schématu pro výpočet nejistoty odhadované doby příletu. Současně je zde vysvětlena funkce ostatních bloků pro plánování letu, předpověď počasí, kombinování větrů a výpočet odhadnuté doby příletu a její nejistoty.
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Ricks, Wendell R. "Knowledge-Based System for Flight Information Management." W&M ScholarWorks, 1990. https://scholarworks.wm.edu/etd/1539625650.

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Bertrand, Allison R., Michael S. Moore, and Ben A. Abbott. "System Management in Network-Based Telemetry Systems." International Foundation for Telemetering, 2008. http://hdl.handle.net/10150/606174.

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ITC/USA 2008 Conference Proceedings / The Forty-Fourth Annual International Telemetering Conference and Technical Exhibition / October 27-30, 2008 / Town and Country Resort & Convention Center, San Diego, California
Network-based telemetry systems are increasingly being used to improve the flexibility and longevity of flight test systems. Modern network-based flight test systems utilize large numbers of devices including high-speed network switches, data acquisition devices, recorders, and telemetry interfaces, all of which must be managed in a coordinated fashion. The move to network-based testing provides the ability to build a standards-based System Management interface which can status and control a diverse set of devices. The benefits include the ability to easily tailor System Management tools to support many different styles of user interactions and to quickly integrate new types of devices. While the new capabilities presented by System Management are exciting, the very openness of the system presents challenges to ensure that future growth will be seamlessly supported. This paper will discuss issues encountered while implementing flight test System Management tools for a network-based telemetry system.
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Noonan, Patrick J., Austin J. Whittington, Hakima Ibaroudene, and Myron L. Moodie. "RAPIDLY RECONFIGURABLE SYSTEM MANAGEMENT." International Foundation for Telemetering, 2017. http://hdl.handle.net/10150/627018.

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The growth of network and distributed technologies in flight test instrumentation (FTI) has provided the benefits of flexibility, scalability, and compatibility with prevalent computing capabilities. However, to achieve these capabilities, the complexity of each piece of FTI and the overall system has increased dramatically. Even with systems composed of equipment from a single vendor, it is important to have management systems that provide the flexibility to adapt quickly to various system configurations and present unified information to the flight test users. The growth of network technologies and then standardized approaches such as iNET standards becoming accepted IRIG 106 standards is leading to the growth of multi-vendor systems. These multi-vendor systems further increase the need for rapidly reconfigurable management systems. This paper describes a constraints engine we have developed to enable flexible system management systems and reflects on how these techniques have been used successfully in the iNET System Manager.
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Crenwelge, Robert, Brian Conway, and Kevin Dillon. "ENTERPRISE FLIGHT DATA MANAGEMENT SYSTEM (EFDMS) AND STORAGE INFRASTRUCTURE TECHNOLOGY DISCUSSION." International Foundation for Telemetering, 2002. http://hdl.handle.net/10150/607565.

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International Telemetering Conference Proceedings / October 21, 2002 / Town & Country Hotel and Conference Center, San Diego, California
This paper presents efforts in developing a data management system and storage infrastructure for assisting test engineers in achieving information superiority and maintaining vital up-to-date information. The focus of this Paper is to generate support for a technology refresh, upgrading the major data centers that share in the responsibility of processing telemetry information. We illustrate how our efforts fit into this goal and provide an overview of our concept for a revolutionary transformation in data management systems. We present the significance of this new technology and suggest a path to implementing the solution.
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Lammers, Zachary A. "Thermal Management of Electromechanical Actuation System for Aircraft Primary Flight Control Surfaces." University of Dayton / OhioLINK, 2014. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1399021324.

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MacInnis, Daniel V. 1964. "Development of a system dynamics based management flight simulator for new product development." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/34732.

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Thesis (S.M.)--Massachusetts Institute of Technology, System Design & Management Program, 2004.
Includes bibliographical references (p. 152-153).
All firms in any mature product development industry are being pressured into performing 'better, faster, and cheaper' by both customers and competitors. In short, firms are being tasked with doing more, with less, faster. This leads to product development organizations being unrealistically tasked to deliver on these programs that often lead to projects falling behind schedule, over budget, and with inadequate quality. While striving to do the right actions to survive, the management of these firms may be leading their firms to disaster through over commitment, and short-term management actions to address the quality, budget, and schedule shortfalls. An understanding of the system dynamics associated with the program management of new product development (NPD) programs is essential to reversing this trend. Several corporations are instituting system dynamics in their management and executive training curricula to affect correct policies, procedures, and behaviors that lead to success. However, because the correct policies, procedures, and behaviors as revealed by system dynamics analysis are counter-intuitive and opposite those policies currently employed in program management, a method is needed to drive the learning of system dynamics so that it becomes ingrained in the program management thought processes. A management flight simulator (MFS) of the program management of a new product development project based on system dynamics provides the hands on experience that managers can learn the consequences of non systems-thinking policies on project performance and how system dynamics based policies can lead to greater success. This thesis provides an overview of the system dynamics of project management in new product development and insight into the
(cont.) correct policies, procedures, and behaviors that lead to success. Research on the role of MFSs in driving the learning of system dynamics principles is explored. A single-phase system dynamics model for a new product development program and a MFS is developed to teach the fundamental lessons of system dynamics applied to product development project management and is to be incorporated in the BP Project Academy. Insight from my own experiences in product development is incorporated in this MFS as well as in recommendations for further development.
by Daniel V. MacInnis.
S.M.
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Lamb, Timothy G. "Future small unmanned aerial system (SUAS) flight and mission control support system (FMCSS) design." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://handle.dtic.mil/100.2/ADA457224.

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Thesis (M.S. in Information Technology Management)--Naval Postgraduate School, September 2006.
Thesis Advisor(s): Baer, Wolfgang. "September 2006." Includes bibliographical references (p. 99). Also available in print.
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Pan, Jing. "Development of ground station display and flight management system for low-cost vehicle." Thesis, Cranfield University, 2011. http://dspace.lib.cranfield.ac.uk/handle/1826/6288.

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Nowadays, with the development of electronic and communication technologies, more and more low-cost vehicles such as small, light-weight aircraft are widely applied in all kinds of fields. Ground Station is an essential part of low cost vehicles for the operator to control and monitor the vehicles. In this thesis, Ground Station Display and Flight Management System for Low-Cost Vehicles have been developed.The major objective of this project is to design an intuitive and easy operative Human Machine Interface for displaying and monitoring the flight data and traffic information on ground. Meanwhile, a Graphic User Interface for the Flight Management System has been developed for realizing the waypoints input and flight plan for the vehicles. To fulfill this task, a low-cost hardware and software architecture is presented. Moreover, some COTS tools such as VAPS and MATLAB are applied for the software development because of their Object-Oriented and Rapid Prototype design methods. At the end of project, simulation has been done for the display HMI to test the behaviours of objects and the impacts of display. The trajectory simulation of flight management control panel is also implemented to test the waypoints creation, trajectory generation and smoothing.
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Moussaddy, Abdel-Rahman. "A thrust controller for the dynamic test bed of the flight management system." Mémoire, École de technologie supérieure, 2009. http://espace.etsmtl.ca/71/1/MOUSSADDY_Abdel%2DRahman.pdf.

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Nous presentons dans cette etude le systeme de controle de la poussee d'un avion civil, le Boeing 747. Le systeme propose, couple a I'autopilote et le systeme de gestion de vol, assure un control automatique de la poussee avec un minimum d'interaction par le pilote. Dans le but de minimiser les frais de developpement CMC developpe un banc d'essai pour leur famille de systemes de gestion de vol (FMS). Ce banc d'essai est utilise comme outil de test, certification et demonstration. Le but du present projet et de developper le systeme de controle de la poussee et de I'integrer au banc d'essai, tout en le qualifiant comme outil de test faisant partie du banc. Afin de pouvoir qualifier le banc d'essai comme outil de tests, plusieurs etapes rigoureuses doivent etre considerees durant le developpement des composantes du banc d'essai, dont le controleur de poussee fait parti. Parmi ces etapes nous retrouvons 1'identification des requis, la proposition du design qui satisfait ces requis, et finalement les tests de validation du systeme selon les exigences initiales, le tout dans un environnement controle. La tache primaire du controleur etant d'assurer une commande de poussee en utilisant la manette de gaz, il est necessaire que le controleur permette de poursuivre une commande de poussee et ce, sans depassement ni erreur en regime permanent. Puisque la poussee n'est pas une entite mesurable directement, nous utilisons un ratio entre la pression a 1'entree et la pression a la sortie des turbines (Engine Pressure Ratio -EPR-) comme mesure de la force appliquee. De plus, couple a I'autopilote, le controleur doit pouvoir poursuivre une commande de vitesse a I'aide du controle de la poussee, et ce sans affecter I'altitude de r avion. Or, une variation de vitesse entraine necessairement une variation de portance et done une variation d'altitude. II est done necessaire de coupler le controle de la poussee au controle de tangage de I'autopilote pour minimiser les variations d'altitudes durant les variations de poussee. Afin d'assurer une securite accme, les limites de vitesses, de poussee ainsi que d'acceleration doivent etre respecte. Finalement le controleur doit etre valide sur I'enveloppe de vol entiere. L'integration du systeme de commande est faite sur le banc de test dynamique developpe par CMC Electronique et ses partenaires. Cette integration ajoute done un requis, soit la necessite que le systeme soit compatible avec la plateforme et qu'il soit developpee en langage C. Deux architectures de controles sont etudiees. Premierement le systeme est developpe en utilisant un controleur Proportioimel-Integral-Derivee (PID) classique et validee sur I'enveloppe de vol entiere. Le controleur utilise deux boucles de controle PID independante, une pour le controle de la poussee et une pour le controle de la vitesse. La selection entre les differentes boucles de controle est faite selon le mode d'autopilote choisi. En mode montee ou descente, comme au decollage, le controleur commande la poussee pour assurer une variation d'altitude pendant que I'autopilote controle la vitesse en utilisant les elevateurs. Une fois que I'altitude desiree est atteinte, le controleur de poussee a le mandat de controler la vitesse tandis que I'autopilote, toujours en utilisant une commande de tangage sur Tangle des elevateurs, assure le maintien de I'altitude. Durant la transition entre ces deux phases de vols d'importantes variations de poussee sont observees. Cette variation cause une variation d'altitude, et une importante acceleration, qui est ensuite armulee par la commande de tangage. Pour pouvoir assurer une transition douce sans variation d'altitude la commande de poussee et la commande de tangage sont couplees. Nous proposons une commande de poussee proportioimelle a la variation d'aUitude pour assurer une transition lisse. Le gain dans la boucle de controle de vitesse est done proportionnel a la variation d'altitude. La deuxieme architecture propose un controleur modeme a retour d'etat qui couple vitesse et tangage. Cette architecture n'utilise pas de boucles independantes et done permet d'assurer un controle en utilisant les elevateurs et la poussee conjointement pour atteindre une altitude et vitesse dormee. Cela permet d'eviter les variations d'altitude dues aux variations de vitesse ainsi que les variations de vitesse dues aux variations d'angle de tangage. Les gains de retour d'etats sont calcules par placement de vecteurs propres pour assurer la robustesse du systeme. Un controleur distinct a ete valide pour differentes positions de I'enveloppe de vol et le systeme de controle selectionne les gains du controleur selon la zone de I'enveloppe de vol courante. Plusieurs autres ameliorations ont ete apportees aux deux architectures pour assurer la protection des limites dynamiques de vitesses et poussees. L'integration du controleur a retour d'etat, systeme de commande moderne, au banc d'essai tut impossible du aux limitations de I'autopilote et de la plateforme de developpement. Cette integration necessite une action directe sur la manette des gaz et sur les elevateurs. Cependant, une loi de commande des elevateurs inteme est incorporee dans la plateforme et les elevateurs sont controles via I'angle de tangage seulement. Pour pouvoir acceder directement a Tangle des elevateurs une modification a la plateforme doit etre effectue ce qui tombe malheureusement a Texterieur des limites de cette etude. Cependant le controleur classique fut integre et teste. Pour qualifier le controleur comme outil de test et developpement integre sur le banc d'essai il a fallu demontrer le respect des exigences et Tatteinte de la performance desiree. Plusieurs tests ont ete ecrits a cette fin et les resultats ont ete concluants. Le controleur assure une poursuite de poussee et de vitesse sans depassement ni erreur en regime permanent. II permet aussi de poursuivre une vitesse sans affecter I'altitude. Les contraintes de vitesse, de poussee et d'acceleration sont de plus respectees. Plusieurs ameliorations possibles sont aussi presentees pour ameliorer le respect des limites de vitesses durant les manoeuvres de poursuite de poussee.
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Books on the topic "Flight management system"

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FEDERAL AVIATION ADMINISTRATION. Flight Management System (FMS) instrument procedures development. [Washington, D.C.?]: U.S. Dept. of Transportation, Federal Aviation Administration, 1996.

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Caballero, Ricardo J. Financial system risk and flight to quality. Cambridge, MA: Massachusetts Institute of Technology, Dept. of Economics, 2005.

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Bever, Glenn A. The development of an airborne information management system for flight test. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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International Aviation Safety Conference (1997 Rotterdam, Netherlands). Aviation safety: Human factors, system engineering, flight operations, economics, strategies, management. Edited by Soekkha Hans M. Utrecht: VSP, 1997.

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Larson, Richard R. AFTI/F-111 MAW flight control system and redundancy management description. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1987.

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Larson, Richard R. AFTI/F-111 MAW flight control system and redundancy management description. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1987.

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Larson, Richard R. AFTI/F-111 MAW flight control system and redundancy management description. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1987.

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Larson, Richard R. AFTI/F-111 MAW flight control system and redundancy management description. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1987.

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Rivers, Timothy C. Design and integration of a Flight Management System for the unmanned air vehicle FROG. Monterey, Calif: Naval Postgraduate School, 1998.

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Kudryakov, Sergey, Valeriy Kul'chickiy, Nikolay Povarenkin, Viktor Ponomarev, Evgeniy Rubcov, and Evgeniy Sobolev. Radio engineering support of aircraft flights and aviation telecommunications. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/1242223.

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The training manual describes the basics of radio engineering support for flights, the organization of radio engineering support for flights, and the general characteristics of flight support equipment. Information is provided about drive radios, marker beacons, radio beacon landing systems, automatic direction finders, RSBN system, VOR and DME beacons, satellite navigation systems, as well as radar surveillance equipment. The basics of telecommunications, issues of aviation telecommunications, as well as information about the means of aviation telecommunications are presented. There are questions for self-control. It is intended for students studying under the specialty program in the specialty 25.05.05 "Aircraft operation and air traffic management"; for students studying under the bachelor's program in the direction of training 25.03.04 "Airport operation and aircraft flight support", as well as for students studying under the master's program in the direction 25.04.04 "Airport Operation and aircraft flight support".
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Book chapters on the topic "Flight management system"

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Zimpfer, Douglas J. "Flight Control Health Management." In System Health Management, 483–95. Chichester, UK: John Wiley & Sons, Ltd, 2011. http://dx.doi.org/10.1002/9781119994053.ch30.

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Jouhaud, Frank. "Flight Path Management System of EOLE UAV." In Advances in Aerospace Guidance, Navigation and Control, 119–34. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_8.

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Ollivier-Legeay, Hortense, Abdessamad Ait El Cadi, Nicolas Belanger, and David Duvivier. "A 4D Augmented Flight Management System Based on Flight Planning and Trajectory Generation Merging." In Towards Autonomous Robotic Systems, 184–95. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-63486-5_21.

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Teng, Liqiang, Wenshan Wang, and Yining Liu. "Architecture Design of High Safety Helicopter Flight Control System with Direct Control Mode." In Complex Systems Design & Management, 473. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-73539-5_40.

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Shen, Jieshi, Bingfei Li, and Cong Chen. "Design of Test Flight Mission Planning and Playback Verification System Based on STK." In Complex Systems Design & Management, 227–40. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-73539-5_18.

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Xi, Wu Chen, and Kazuhiro Aoyama. "A Support System for Flight Service Management Based on Service Model." In Concurrent Engineering Approaches for Sustainable Product Development in a Multi-Disciplinary Environment, 645–56. London: Springer London, 2012. http://dx.doi.org/10.1007/978-1-4471-4426-7_55.

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Ma, Cunbao, Ying Wang, and Wen Li. "Design and Implementation of a Flight Data Ground Analysis System." In Proceedings of the First Symposium on Aviation Maintenance and Management-Volume I, 343–51. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54236-7_39.

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Song, Dong, and Bin Han. "Avionic Fault Diagnosis Expert System Based on Flight Data and BIT Information." In Proceedings of the First Symposium on Aviation Maintenance and Management-Volume I, 303–11. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54236-7_34.

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Ma, Wenlai, Shouxi Zhu, and Hongfang Xue. "Design and Simulation of a Kind of Unmanned Helicopter Fixed-Altitude Flight Control System." In Proceedings of the First Symposium on Aviation Maintenance and Management-Volume I, 269–78. Berlin, Heidelberg: Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-54236-7_30.

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Leva, Maria Chiara, Alison Kay, Joan Cahill, Gabriel Losa, Sharon Keating, Diogo Serradas, and Nick McDonald. "Unique Reporting Form: Flight Crew Auditing of Everyday Performance in an Airline Safety Management System." In Lecture Notes in Computer Science, 806–15. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-02559-4_87.

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Conference papers on the topic "Flight management system"

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Wichman, Keith D., Joel K. Klooster, Okko F. Bleeker, and Richard M. Rademaker. "Flight validation of downlinked flight management system 4D trajectory." In 2007 IEEE/AIAA 26th Digital Avionics Systems Conference. IEEE, 2007. http://dx.doi.org/10.1109/dasc.2007.4391833.

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Lin, Gene, Mushava Kodzwa, Mahesh Balakrishna, and Gerry McNeill. "Characterization of Flight Management System (FMS) Intent from Operational Flights." In 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-9141.

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MORGER, K. "Computer aided requirements management system (CARMS) and flight test." In 4th Flight Test Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2091.

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Park, Sang Gyun, Veera V. Vaddi, and Jason Kwan. "Next Generation Flight Management System Simulator." In AIAA Modeling and Simulation Technologies Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-0425.

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Zheng, Jiawei, and Lichen Zhang. "AADL-Based Flight Management System Modeling." In 2018 International Conference on Network, Communication, Computer Engineering (NCCE 2018). Paris, France: Atlantis Press, 2018. http://dx.doi.org/10.2991/ncce-18.2018.129.

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Howells, Peter J., and Donald Moore. "Flight Management Computer System Datalink Interface Capabilities." In Aerospace Technology Conference and Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1990. http://dx.doi.org/10.4271/901954.

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COMBS, S., A. SANCHEZ-CHEW, and G. TAUKE. "Flight management system integration on the F-117A." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1077.

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Deng, Lei, and De-yuan Gao. "Design of Flight Service Vehicle Dispatching Management System." In 2009 International Conference on Communication Software and Networks. IEEE, 2009. http://dx.doi.org/10.1109/iccsn.2009.36.

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Sikora, Adam, and Roman Czyba. "Independent Flight Management System for Unmanned VTOL Aircraft." In 2018 23rd International Conference on Methods & Models in Automation & Robotics (MMAR). IEEE, 2018. http://dx.doi.org/10.1109/mmar.2018.8486095.

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Tseng, Kuo-Hsiung, Kuo-Hui Chen, and Chih-Lin Chu. "Design and implementation of flight information management system." In 2016 IEEE 11th Conference on Industrial Electronics and Applications (ICIEA). IEEE, 2016. http://dx.doi.org/10.1109/iciea.2016.7603552.

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Reports on the topic "Flight management system"

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Emmitt, George D., Steven Greco, and Sidney Wood. In-flight Integrated Mission Management System (I-LIMMS). Fort Belvoir, VA: Defense Technical Information Center, December 2006. http://dx.doi.org/10.21236/ada462225.

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Seybold, Patricia. Designing a Customer Flight Deck(SM) Performance Management System. Boston, MA: Patricia Seybold Group, October 2001. http://dx.doi.org/10.1571/ov10-25-01cc.

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Doo, Johnny. Unsettled Issues Concerning the Opportunities and Challenges of eVTOL Applications during a Global Pandemic. SAE International, October 2020. http://dx.doi.org/10.4271/epr2020022.

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Abstract:
Electric vertical takeoff and landing (eVTOL) aircraft technology has developed beyond the traditional aviation industry and now influences the creation of new and novel transportation applications. Some experts even suggest on-demand eVTOL logistics capabilities could be harnessed by crisis response teams to c ombat a future pandemic. The lessons of the COVID-19 crisis highlighted the challenges of managing a global pandemic response due to the difference in regional and local resources, culture, and political systems. Although there may not be a uniform crisis management strategy that the world can agree on, next-generation vertical flight vehicles could be used to distribute limited medical equipment, supplies, and personnel to hot spots faster than conventional aircraft or ground vehicles. However, creating this capability is not easy. This SAE EDGE™ Research Report by Johnny Doo addresses the opportunities and challenges of establishing an eVTOL fleet, including deployment, supporting infrastructure, and fleet management.
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NASA Marshall Space Flight Center Improves Cooling System Performance: Best Management Practice Case Study #10: Cooling Towers (Fact Sheet). Office of Scientific and Technical Information (OSTI), February 2011. http://dx.doi.org/10.2172/1008190.

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