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1

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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2

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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3

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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4

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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5

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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6

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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7

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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8

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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9

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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10

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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11

Palacios, Rafael, and R. John Hansman. "Filtering Enhanced Traffic Management System (ETMS) Altitude Data." Metrology and Measurement Systems 20, no. 3 (September 1, 2013): 453–64. http://dx.doi.org/10.2478/mms-2013-0039.

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Abstract Enhanced Traffic Management System (ETMS) stores all the information gathered by the Federal Aviation Administration (FAA) from aircraft flying in the US airspace. The data stored from each flight includes the 4D trajectory (latitude, longitude, altitude and timestamp), radar data and flight plan information. Unfortunately, there is a data quality problem in the vertical channel and the altitude component of the trajectories contains some isolated samples in which a wrong value was stored. Overall, the data is generally accurate and it was found that only 0.3% of the altitude values were incorrect, however the impact of these erroneous data in some analyses could be important, motivating the development of a filtering procedure. The approach developed for filtering ETMS altitude data includes some specific algorithms for problems found in this particular dataset, and a novel filter to correct isolated bad samples (named Despeckle filter). As a result, all altitude errors were eliminated in 99.7% of the flights affected by noise, while preserving the original values of the samples without bad data. The algorithm presented in this paper attains better results than standard filters such as the median filter, and it could be applied to any signal affected by noise in the form of spikes
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12

Barfield, Carl S., Deborah J. Waters, and Howard W. Beck. "Flight Device and Database Management System for Quantifying Insect Flight and Oviposition." Journal of Economic Entomology 81, no. 5 (October 1, 1988): 1506–9. http://dx.doi.org/10.1093/jee/81.5.1506.

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13

Pita, Javier Losada, and Félix Orjales Saavedra. "UAV Trajectory Management: Ardupilot Based Trajectory Management System." Proceedings 21, no. 1 (July 23, 2019): 8. http://dx.doi.org/10.3390/proceedings2019021008.

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In this paper we explain the structure and development of a trajectory management system on board a UAV capable to achieve complex trajectories and versatile to adapt disturbances during flight. This system is built in Python and runs in a companion computer on board the UAV while maintains communication with a ground station over a radio link.
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14

Sainthuile, Gerard. "The future functionalities of the flight management system." Air & Space Europe 1, no. 1 (January 1999): 51–54. http://dx.doi.org/10.1016/s1290-0958(99)80039-2.

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15

Dan, GULTUREANU, KERNS Kevin, HENTHORN Tom, QUACH John, and KLEEN Mitch. "Flight Software Development and Validation Workflow Management System." INCAS BULLETIN 10, no. 1 (March 11, 2018): 85–94. http://dx.doi.org/10.13111/2066-8201.2018.10.1.9.

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16

Park, Sung-Han, Jae-Yong Kim, In-Je Cho, and Byung-Moon Hwang. "Redundancy Management Design for Triplex Flight Control System." Journal of the Korean Society for Aeronautical & Space Sciences 38, no. 2 (February 1, 2010): 169–79. http://dx.doi.org/10.5139/jksas.2010.38.2.169.

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17

Mohleji, S. C. "Optimal flight management system utilization with ATC automation." IEEE Aerospace and Electronic Systems Magazine 4, no. 2 (February 1989): 26–32. http://dx.doi.org/10.1109/62.16993.

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18

Sherry, Lance, and Peter G. Polson. "Shared Models of Flight Management System Vertical Guidance." International Journal of Aviation Psychology 9, no. 2 (April 1999): 139–53. http://dx.doi.org/10.1207/s15327108ijap0902_4.

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19

Salden, Ron J. C. M., Fred Paas, Jelke van der Pal, and Jeroen J. G. van Merrienboer. "Dynamic Task Selection in Flight Management System Training." International Journal of Aviation Psychology 16, no. 2 (April 2006): 157–74. http://dx.doi.org/10.1207/s15327108ijap1602_3.

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20

Bachkalo, B. I., and V. I. Zolotykh. "The possibility of the event-based flight safety control taking into account the particular qualities of the pilot." Civil Aviation High Technologies 23, no. 4 (September 4, 2020): 8–19. http://dx.doi.org/10.26467/2079-0619-2020-23-4-8-19.

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The article analyzes the flight safety management process. The structure of the flight safety management system and the subjectobject interaction which is in the base of this system functioning are shown. The necessity of aircraft intelligent on-board control systems development and implementation is proved. The tasks that such systems will allow to solve during the flight are outlined. Application prospects of the real and documented flight safety contours in the system of active flight safety management are considered. The possibility of active flight safety control based on the parametric control principle is shown. The necessity of flight safety management based on the event-based control principle with the use of documented flight safety contour is proved. The example which visually demonstrates the capabilities and prospects of event-based flight safety management has been considered. The necessity of a particular pilot psychical characteristics taking into account while forming the contour of documented flight safety is proved. For this purpose, the flight personnel mental state systematic monitoring with the aim of professional suitability indicator determination expediency is justified. The possibility of using the pilot’s personal database for documented safety contour formation of each specific flight is considered in order to take into account the features of a particular pilot in managing flight safety. This should be a self-learning system that operates on the basis of the neural networks application and allows you to take into account all the characteristic and temperament features of each pilot in person. It is proved that the possibility of the pilot’s mental state taking into account, expressed by the value of the professional suitability indicator, can be successfully implemented exactly in the event of flight safety management, which will lead to the security increase of the aviation system from exposure of hazardous factors during the flight mission.
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21

Puzio, Łukasz, Mateusz Milewski, Robert Sklorz, and Arkadiusz Tofil. "Unstabilized approach in aviation training on the basis of the fliight data monitoring (FDM4GA)." Transportation Overview - Przeglad Komunikacyjny 2018, no. 12 (December 1, 2018): 1–6. http://dx.doi.org/10.35117/a_eng_18_12_01.

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The article takes up the issue based on flight monitoring systems (FDM) in the aspect of aviation training. The key element is the use of Storkjet software and data recorded on flight recorders from the Aviation Training Center (OKL) of the State School of Higher Education in Chełm. The authors of the article have adopted a model of an approach path including air regulations, aircraft performance based on Aircraft Flight Manual (AFM), procedures based on OKL’s the Standard Operating Procedures (SOPs) and navigation data based on approved navigation information for specific airports. The problem of unstabilized approaches has been analyzed on the basis of data from various flight groups (e.g. instrument flights, night flights, etc.). As a result, flight groups were selected, which statistically from the point of view of the risk management system bring the largest operational risk during the aviation education process.
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22

Kavitha, V., and Agnus S. Swarnanisha Lakshmi. "Wireless system for flight safety industry." International Journal of Enterprise Network Management 9, no. 3/4 (2018): 227. http://dx.doi.org/10.1504/ijenm.2018.094661.

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23

Lakshmi, Agnus S. Swarnanisha, and V. Kavitha. "Wireless system for flight safety industry." International Journal of Enterprise Network Management 9, no. 3/4 (2018): 227. http://dx.doi.org/10.1504/ijenm.2018.10015773.

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24

Sherry, Lance, Karl Fennell, Michael Feary, and Peter Polson. "Human-Computer Interaction Analysis of Flight Management System Messages." Journal of Aircraft 43, no. 5 (September 2006): 1372–76. http://dx.doi.org/10.2514/1.20026.

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25

Kaptsov, Maxim, and Luis Rodrigues. "Flight management system for hydrogen-powered aircraft in cruise." Aerospace Systems 4, no. 3 (June 14, 2021): 201–8. http://dx.doi.org/10.1007/s42401-021-00097-8.

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26

Pakdil, M. E., R. N. Celik, Ö. Kaya, Y. C. Konak, and C. Guney. "SMART AERONAUTICAL CHART MANAGEMENT SYSTEM DESIGN." ISPRS Annals of Photogrammetry, Remote Sensing and Spatial Information Sciences II-2/W2 (October 19, 2015): 83–87. http://dx.doi.org/10.5194/isprsannals-ii-2-w2-83-2015.

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Civil aviation is developing rapidly, and the number of domestic and international operations is increasing exponentially every year than the previous one. Airline companies with increased air traffic and the number of passengers increase the demand of new aircrafts. An aircraft needs not only fuel but also pilot and aeronautical information (charts, digital navigation information, flight plan, and etc.) to perform flight operation. One of the most important components in aeronautical information is the terminal chart. Authorized institution in every state is responsible to publish their terminal charts for certain periods. Although these charts are produced in accordance with ICAO’s Annex 4 and Annex 15, cartographic representation and page layout differs in each state’s publication. This situation makes difficult to read them by pilots. In this paper, standard instrument departure (SID) charts are analysed to produce by use of cutting-edge and competitive technologies instead of classical computer-aided drawing and vector based graphic applications that are currently used by main chart producers. The goal is to design efficient and commercial chart management system that is able to produce aeronautical charts with same cartographic representation for all states.
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27

Chaves, Filipe. "Airline safety management system issues: a practitioner’s perspective." Aircraft Engineering and Aerospace Technology 92, no. 2 (November 17, 2019): 117–27. http://dx.doi.org/10.1108/aeat-11-2018-0280.

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Purpose This study aims to introduce the reader to some problems faced by safety practitioners operating within an airline safety department, particularly risk assessment subjectivity, and processing of flight data monitoring events. In doing so, it attempts to propose solutions to these issues. Design/methodology/approach Quality management tools, including six sigma, in combination with flight data monitoring, are proposed as a solution to the issues identified. Findings The proposed solutions reduce the subjectivity of some risk assessments and help airlines to efficiently process flight data monitoring events. Research limitations/implications This paper presents a two-part case study of how these issues have been dealt with by an airline. However, as demonstrated by the literature review, there seems to exist further advanced methods, some of them still in a developmental stage, to deal more effectively with the problems discussed. Originality/value This study is particularly directed and more valuable to small-scale airlines. These are more susceptible to the lack of resources needed to implement advanced approaches into the safety management system, but still want to adopt a systematic way of conducting business. Furthermore, it highlights common issues faced by safety practitioners in airlines and should hopefully stimulate the discussion around the topic and promote other academics/practitioners to share viable solutions.
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28

Szafrański, Bolesław, Mirosław Zieja, Jarosław Wójcik, and Krzysztof Murawski. "Data analysis of information system TURAWA in the aspect of data mining methods." Computer Science and Mathematical Modelling, no. 7/2018 (July 18, 2018): 45–52. http://dx.doi.org/10.5604/01.3001.0012.2004.

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The article is devoted to the analysis of data coming from the operation process and collected in computer system TURAWA, which focuses on supporting the management of flight safety in the Polish Air Force. The Armed Forces are equipped with a system, which collects and processes data concerning the whole air crew, all performed flights and all aircraft. The increasing opportunities in obtaining data and the continuous development of data mining methods allow to extract information never been known before, which, together with conclusions obtained from the data analysis, will help to improve the level of flight safety.
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29

Amaro Carmona, Manuel Angel, Darius Rudinskas, and Cristina Barrado. "DESIGN OF A FLIGHT MANAGEMENT SYSTEM TO SUPPORT FOUR-DIMENSIONAL TRAJECTORIES." Aviation 19, no. 1 (March 30, 2015): 58–65. http://dx.doi.org/10.3846/16487788.2015.1015284.

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This paper presents the design and simulation of the functions of a flight Management System (FMS) in order to follow four-dimensional trajectories automatically. This is achieved by controlling the aircraft’s airspeed, altitude, heading and vertical speed in order to arrive to the merging point in a specified time. The system receives data from the aircraft and computes new control parameters based on mathematical equations and algorithms of prediction trajectories. Additional features have been added to the FMS-4D, such as the capability of predicting the arrival time taking into account previous flight parameters and speed/altitude constrains. Finally, a testing phase was carried out using a flight simulator in order to obtain the performance and results of the designed system.
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30

Zieja, Mariusz, Henryk Smoliński, and Paweł Gołda. "Proactive methods – new quality in aircraft flight safety management." Journal of KONBiN 36, no. 1 (December 1, 2015): 105–14. http://dx.doi.org/10.1515/jok-2015-0060.

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Abstract This article reviews methods that apply in data and information analysis on flight safety and also was made a review of the features and examples of system resources of proactive management of flight safety. It proposes a general methodology for IT support of proactive flight safety management in the form of an algorithm, whose individual elements been described. Was presented an example of the application of the algorithm, selected methods and tools for data analysis and identification of corrective and/or preventive actions, as part of flight safety management and the monitoring of their effectiveness and efficiency through continuous analysis and assessment of data and information from the system, as an element of flight safety management. This article presents a methodological approach to the analysis and assessment of the risks to flight safety with regard to proactive processes
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31

Gan, Xu Sheng, Hao Lin Cui, and Ya Rong Wu. "Study on Mechanical Engineering for Flight with Flight Safety Evaluation Method on Relevance Vector Machine." Applied Mechanics and Materials 454 (October 2013): 70–73. http://dx.doi.org/10.4028/www.scientific.net/amm.454.70.

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The mechanical engineering for flight are important for flight safety to prevent the flight accident, improve the management and decision-making level of flight safety. In order to improve the safety of flight system, a flight safety evaluation method based on relevance vector machine and flight mechanical engineering is proposed. First, based on system viewpoint, according to the actual situation of flight safety, the factors that influence the safety of flight system are found out on four sides of human, flight mechanical engineering, environment and management and the flight safety evaluation index system is constructed; then the flight safety evaluation model based on relevance vector machine developed in the framework of Bayesian theory is briefly introduced; finally using the index system the relevance vector machine evaluation model of flight safety is establish. The actual example confirms its feasibility.
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32

Tuân, Lê Đình, Anh Trần Tiến, and Hải Nguyễn. "On the airport environmental noise monitoring and control system." Science & Technology Development Journal - Engineering and Technology 3, SI2 (January 23, 2021): first. http://dx.doi.org/10.32508/stdjet.v3isi2.622.

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Most major airports use permanent noise and operations monitoring systems to reduce the noise of flight operations in the surrounding community. This paper aims at a technical proposal for a permanent environmental noise monitoring and control system to provide solutions to reduce the noise of flying activities for communities around the airport. Airport noise monitoring is often used to evaluate noise abatement programs and to improve the aircraft's take-off / landing procedures, to minimize the impact of aircraft noise based on altitude, flight path and time of day. Noise monitoring is usually linked to the tracking radar to determine which aircraft is in particular when the noise limit is exceeded and thus provides immediate operational requirements to meet. The airport noise enviromental monitoring and control system is often structured with fixed permanent noise monitoring stations, mobile noise monitoring stations, multi-parameter wheather stations, radar tracks and flights information to automatically evaluate the noise impact due to operation of aircrafts in the surrounds of airport, near and on residential areas. The entire system is operated by a software platform proposed as a cloud configuration available on the internet. The platform provides all the modules required to manage data such as noise and flight information monitoring and control, live data, reports, noise and flight information in public disclosure, complaints management, alarms and warnings, etc.
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33

Moore, P., and D. M. Page. "The Delco Performance Management System." Journal of Navigation 38, no. 3 (September 1985): 413–22. http://dx.doi.org/10.1017/s037346330003277x.

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Since the early nineteen-seventies, when the price of fuel went up so dramatically, airlines have been seeking methods of saving fuel. Climb, cruise and descent speeds were refined to give the most economical operation. Advisory systems came on the market, but these did little more than give crews information which could be obtained from operations manuals. Then equipment such as performance management systems (PMS) and flight management systems (FMS) was produced. The potential of these systems can be measured by the number of airlines who have purchased the equipment, and also by the fact that most of the new generation of aircraft are being built with PMS as part of the standard aeroplane.
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34

Schutte, Paul C., and Anna C. Trujillo. "Flight Crew Task Management in Non-Normal Situations." Proceedings of the Human Factors and Ergonomics Society Annual Meeting 40, no. 4 (October 1996): 244–48. http://dx.doi.org/10.1177/154193129604000422.

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Task management (TM) is always performed on the flight deck, although not always explicitly, consistently, or rigorously. Nowhere is TM as important as it is in dealing with non-normal situations. The objective of this study was to analyze pilot TM behavior for non-normal situations. Specifically, the study observed pilots' performance in a full workload environment in order to discern their TM strategies. This study identified four different TM prioritization and allocation strategies: ‘Aviate-Navigate-Communicate-Manage Systems’; ‘Perceived Severity;’ ‘Procedure Based;’ and ‘Event/Interrupt Driven.’ Subjects used these strategies to manage their personal workload and to schedule monitoring and assessment of the situation. The ‘Perceived Severity’ strategy for personal workload management combined with the ‘Aviate-Navigate-Communicate- Manage Systems’ strategy for monitoring and assessing appeared to be the most effective (fewest errors and fastest response times) in responding to the novel system failure used in this study.
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35

Perna, Michael Di, and Luis Rodrigues. "A UAV software flight management system using arinc communication protocols." IEEE Aerospace and Electronic Systems Magazine 33, no. 9 (September 2018): 18–28. http://dx.doi.org/10.1109/maes.2018.170085.

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36

Sangam, Manoj, Roberto Sabatini, Subramanian Ramasamy, and Alessandro Gardi. "Advanced Flight Management System for an Unmanned Reusable Space Vehicle." International Journal of Unmanned Systems Engineering 1, no. 3 (July 1, 2013): 48–67. http://dx.doi.org/10.14323/ijuseng.2013.12.

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37

Lee, Wo-Il, and Jung-Ho Eom. "Development of Pilot’s Condition Measurement System for Flight Safety Management." Journal of Security Engineering 10, no. 5 (October 31, 2013): 539–48. http://dx.doi.org/10.14257/jse.2013.10.5.05.

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38

Tanabe, Toru, Masatoshi Harigae, and Naoji Tomita. "The concept of autonomous flight management system for future spacecraft." Acta Astronautica 16 (January 1987): 3–10. http://dx.doi.org/10.1016/0094-5765(87)90088-9.

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39

Zhang, Honghai, Qiqian Zhang, and Lei Yang. "A User Equilibrium Assignment Flow Model for Multiairport Open Network System." Mathematical Problems in Engineering 2015 (2015): 1–11. http://dx.doi.org/10.1155/2015/631428.

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To reduce flight delays and promote fairness in air traffic management, we study the imbalance problem between supply and demand in airport network system from the view of both the system and the users. First, we establish an open multiairport oriented network flow system with the correlation between the arrival and departure in capacity-constrained airports, as well as the relevance between multiairports united flights. Then, based on the efficiency rationing principle, we propose an optimization model to reassign flow with user equilibrium constraints. These constraints include Gini coefficient, system capacity, and united flights. The model minimizes the total flight delay cost of capacity-constrained airports in the network system. We also introduce some evaluation indexes to quantitatively analyze fairness among airlines. Finally, with an open multiairport network system and its actual flights data in China, the model is verified. Test results show that the model can be used to coordinate and optimize matching the flow and capacity in the multiairport, make full use of the capacity of airports, and minimize the system delays. The findings can provide a powerful reference of developing scientific and rational assignment strategy for air traffic controllers.
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Wang, Yanjun, Hongfeng Zheng, Fan Wu, Jun Chen, and Mark Hansen. "A Comparative Study on Flight Delay Networks of the USA and China." Journal of Advanced Transportation 2020 (June 2, 2020): 1–11. http://dx.doi.org/10.1155/2020/1369591.

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Recent studies have characterized the structures of air transport network in different countries and regions using complex network metrics. These studies coincided with the trend of increasingly available large empirical flight datasets that enable researchers to investigate the dynamics of the system, such as the propagation of flight delay. However, linking network structure with network dynamics remains a challenging task. In this paper, we proposed a method to construct flight delay networks from operational data. We provided a detailed comparison of the key structural properties of the flight delay networks in the United States and China. The comparisons of betweenness centrality of delay networks and flight networks show the advantage of the proposed method. We further found that airports in similar geographical locations do exhibit similar delay patterns in both countries. To explore the underlying mechanisms, the Multifractal Detrended Fluctuation Analysis (MF-DFA) is applied to the flights’ delay time series at both the airport level and network level. Singularity spectra analyses reveal the fundamental characteristics of the airport systems and air transportation system. Our findings contribute to the understanding of structure and dynamics of air transportation systems.
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Ramasamy, Subramanian, Manoj Sangam, Roberto Sabatini, and Alessandro Gardi. "Flight Management System for Unmanned Reusable Space Vehicle Atmospheric and Re-Entry Trajectory Optimisation." Applied Mechanics and Materials 629 (October 2014): 304–9. http://dx.doi.org/10.4028/www.scientific.net/amm.629.304.

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The design and trajectory computation algorithms of an innovative Flight Management System (FMS) for Unmanned Reusable Space Vehicle (URSV) are presented. The proposed FMS features a number of common functionalities with modern aircraft FMS that enable flight planning in non-segregated airspace, as well as specific features for optimal trajectory generation and space segment monitoring of the flight mission. The general avionics architecture of URSV is presented and the specific FMS algorithms are developed to cope with the flight vehicle optimal trajectory planning and monitoring. Simulation case studies are performed in a realistic operational scenario resulting in the rapid generation of feasible trajectories, ensuring no violation of the defined mission and vehicle dynamics constraints. Additionally, error budget analysis is performed on longitudinal profile trajectories to evaluate the URSV performance.
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Muliasari, Ataline. "Upaya Bandara Ngurah Rai Denpasar Dalam Mewujudkan Safety Management System (SMS)." Warta Penelitian Perhubungan 22, no. 5 (May 31, 2010): 481–96. http://dx.doi.org/10.25104/warlit.v22i5.1113.

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Each airport management including Denpasar Ngurah Rai International Airport are required tocreate, implement, eunluate and impmue the sustainnble safe~; rruznagement si;stem (SMS) with asafehJ program based on intemntionnl mzd nntionnl flight s. Relnted to the nhaue, ns nn internationalairport located in the center of touris111 lcxatio11 of hzdonesin, Nguralt Rni lntenuztional Airport tnjingto realize its SafehJ Management System (SMS). Ihis condition is certainly important to be realizedconsidering the level of aircraft mauements for both international and national flights is very high atthis airport. Vvhen considering the results of a questionnaire on the indicators of Hazard Identifica.tionand Risk Management, there are variables that are in the position of" risk control/ mitigation requiresa management decision" that is a wild life nrea airports (VVild Life). T77erefore, Denpasar Ngurah RaiAirport management lzas planned safety targets 11~1/ be nc/1iered within 3 (tlzree) years from 2010through 2012.
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Ramasamy, Subramanian, Roberto Sabatini, Alessandro Gardi, and Trevor Kistan. "Next Generation Flight Management System for Real-Time Trajectory Based Operations." Applied Mechanics and Materials 629 (October 2014): 344–49. http://dx.doi.org/10.4028/www.scientific.net/amm.629.344.

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This paper presents the concept of operations, architecture and trajectory optimisation algorithms of a Next Generation Flight Management System (NG-FMS). The NG-FMS is developed for Four Dimensional (4D) Intent Based Operations (IBO) in the next generation Communications, Navigation, Surveillance and Air Traffic Management system (CNS+A) context. The NG-FMS, primarily responsible for the aircraft navigation and guidance task, acts as a key enabler for achieving higher level of operational efficiency and mitigating environmental impacts both in manned and unmanned aircraft applications. The NG-FMS is interoperable with the future ground based 4DT Planning, Negotiation and Validation (4-PNV) systems, enabling automated Trajectory/Intent Based Operations (TBO/IBO). After the NG-FMS architecture is presented, the key mathematical models describing the trajectory generation and optimisation modes are introduced. A detailed error analysis is performed and the uncertainties affecting the nominal trajectories are studied to obtain the total NG-FMS error budgets. These are compared with the Required Navigation Performance (RNP) values for the various operational flight tasks considered.
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Szabolcsi, Róbert. "Flight Path Planning for Small UAV Low Altitude Flights." Land Forces Academy Review 25, no. 2 (June 1, 2020): 159–67. http://dx.doi.org/10.2478/raft-2020-0019.

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AbstractRecent days there are many projects of UAV urban applications, moreover, although in different habited area. Several concepts like urban drone taxi, flying boards, flying bikes, etc. are in phase of prototype system test and evaluation. As part of the modern robotization, UAVs are in the focus of attention of numerous scientists. UAVs, as special platforms are widely used by the Military in different scenarios and different flight missions. Capabilities of UAVs used in non-military applications (i.e. Police applications, disaster management applications, border control, firefighter applications, etc.) will serve well the idea of UAV 3D (Dirty-Dull-Dangerous) application. The purpose of the author is to derive those low altitude UAV flight regimes when low altitude flight automation in necessary due to flight safety aspects, or, due to any existing regulations, and, finally, find and propose flight paths of the UAV better fitting given mission of the UAV.
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Kondroška, Vaidotas, and Jonas Stankūnas. "ANALYSIS OF AIRSPACE ORGANIZATION CONSIDERING AIR TRAFFIC FLOWS." TRANSPORT 27, no. 3 (September 19, 2012): 219–28. http://dx.doi.org/10.3846/16484142.2012.719199.

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Aviation is one of the most rapidly developing types of transport playing a crucial role in the modern world. Aviation has a sensitive response to any economic or social changes and painful aviation catastrophes. In spite of increasing the flows of passengers and flights, for certain reasons, the aviation system does not always satisfy the expectations of the airspace users in the sense of efficiency. The effectiveness of air transport operations is determined by both a reduction in the costs of every airspace user and the efficiency of the air traffic management system. Airspace organization performed by the air traffic management system, i.e. its adaptation to the performance of appropriate air navigation services, largely defines the efficiency of these services. Due to various reasons, presently, the area of airspace and airspace management has remained one of the largest and incompletely used aviation resources. Beside other appropriate means, the organization of air traffic management and airspace establishes flight conditions and determines the efficiency of flight trajectories and regularity. A comparison of air traffic management systems of different regions identifies the obstacles that do not allow ensuring the maximum results of flight efficiency in any place. One of the main reasons is the high fragmentation of the specified regions that mostly coincide with the state borders. The above reasons show that in order to efficiently develop aviation, the successful development of that to the extent of one country is not enough. Thus, the best results will only be reached solving the existing problems and intended challenges to the extent of a few countries – up to the extent of the whole region. The aim of research is to define a methodology allowing the organization of regional airspace according to the flows of air traffic and subsequently enabling to solve flight efficiency problems related to air traffic management. For space evaluation, the paper suggests using rectangular grids the application of which makes possible dividing the researched space more easily and exactly. Considering the examples of air traffic management systems demonstrating the best results of efficiency, it can be exactly assumed about the number of possible airspace blocks complying with the flows of flights in the analyzed airspace. In case, a preliminary number of the wanted clusters is known, it is purposeful to apply the method of the cluster analysis of K-means with necessary limitations to the formed building airspace blocks and to determine the optimum version taking into account the analyzed ones. The paper suggests representing points having appropriate weighted coefficients during the stage of clustering rather than using grid cells. The optimization of the obtained airspace blocks is necessary in case the formed blocks do not properly comply with the aims raised. The application of the methodology suggested in the paper enables dividing the airspace of a big territory into airspace blocks according to the flows of flights independent from the air way network, flight intensity and the collocation of the airspace elements of a special purpose.
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46

Li, Li Qun. "Analysis on the Architecture of the General Aviation Operation Control System Software." Applied Mechanics and Materials 687-691 (November 2014): 18–21. http://dx.doi.org/10.4028/www.scientific.net/amm.687-691.18.

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General aviation, is refers to the civil aviation activities that is used a civil aircraft engaged in outside of public air transport, including industry, agriculture, forestry, fisheries and homework flight of the construction industry and medical and health, disaster relief, meteorological observation, ocean monitoring, scientific experiment, education and training, culture and sports and other party and flight activities. Therefore, every airline is necessary to set up its own set of flight operation control system. This paper introduces the concept of flight operation control system, system structure and functions of each module, and is given flight operation control system application solutions; provide reference for improving the flight operation and management level in our country.
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Ahmad, Mohamed Tarmizi, Michael Lam, A. S. Mohd Harithuddin, Amzari Zhahir, and Omar Kassim Ariff. "Flight Data Monitoring/Tracker System for Search and Rescue Mission." Applied Mechanics and Materials 629 (October 2014): 350–54. http://dx.doi.org/10.4028/www.scientific.net/amm.629.350.

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<p>Traditionally, Kalman Filter is used for the purpose of mixing several input signals and extracting a more reliable output, which greatly benefits aircraft navigation. This paper considers a fusion of four sensor systems: Global Positioning System (GPS), accelerometer, gyroscope and magnetometer. The resultant device, known as Starfish Main Tracking Unit (MTU), is a Flight Data Monitoring (FDM) / Tracking System equipment that uses General Packet Radio Service (GPRS) / Iridium / ICS (Internet Communications Services), which provides low cost telemetry as well as multiple solutions for global flight following and flight data transfer between aircraft and ground. Users from ground are able to monitor their fleet, configure their systems and also generate various flight reports from a single web-based interface, named the Starfish Fleet Management system. This developed system complements the Black Box by downloading limited aircraft data to the ground, provides real time tracking and assist in Search and Rescue (SAR) mission.</p>
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48

Peng, Kemao. "Autonomous Mission Management Based Nonlinear Flight Control Design for a Class of Hybrid Unmanned Aerial Vehicles." Guidance, Navigation and Control 01, no. 02 (June 2021): 2150009. http://dx.doi.org/10.1142/s2737480721500096.

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In this paper, a nonlinear flight control law is designed for a hybrid unmanned aerial vehicle (UAV) to achieve the advanced flight performances with the autonomous mission management (AMM). The hybrid UAV is capable of hovering like quadrotors and maneuvering as fixed-wing aircraft. The main idea is to design the flight control laws in modules. Those modules are organized online by the autonomous mission management. Such online organization will improve the UAV autonomy. One of the challenges is to execute the transition flight between the rotary-wing and fixed-wing modes. The resulting closed-loop system with the designed flight control law is verified in simulation and the simulation results demonstrate that the resulting closed-loop system can successfully complete the designated flight missions including the transition flight between the rotary-wing and fixed-wing modes.
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49

Rogalski, Tomasz, Andrzej Tomczyk, and Grzegorz Kopecki. "Flight Simulator as a Tool for Flight Control System Synthesis and Handling Qualities Research." Solid State Phenomena 147-149 (January 2009): 231–36. http://dx.doi.org/10.4028/www.scientific.net/ssp.147-149.231.

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At the Department of Avionics and Control Systems problems of aeronautical control systems have been dealt with for years. Several different kinds of aeronautical control systems have been designed, prototyped and tested. These control systems are intended for general aviation aircraft and unmanned aircraft. During all research projects computer simulations and laboratory tests were made. However, since in some cases such tests were insufficient, in-flight tests were conducted leading to a series of reliable results. The in-flight tests were made with the use of M-20 Mewa aircraft (autopilot for a GA aircraft) and PZL-110 Koliber aircraft (control system for UAV and indirect flight control system for a GA aircraft). Nevertheless, in-flight testing is very expensive and problematic. To avoid some problems appearing during in-flight tests and their preparation, a simulator – which is normally used for professional pilot training – can be used. The Aviation Training Center of the Rzeszów University of Technology possesses the ALSIM AL-200 MCC flight simulator. We have started preparing this simulator for the research. It is possible to control the simulated aircraft with the use of an external control system. The solution proposed enables testing the aircraft control algorithms, indirect control laws (e.g. control laws modifying handling qualities), as well as testing and assessment of the students’ pilotage skills. Moreover, the solution makes it possible to conduct tests connected with aircraft control, crew management, crew cooperation and flight safety. The simulator allows us to test dangerous situations, which – because of safety reasons – is impossible during in-flight testing. This paper presents modifications to the simulator’s hardware and additional software, which enable the described research.
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Panggabean, Ellis Mardiana, Herman Mawengkang, M. Zarlis, and Syahril Efendi. "Integer Programming Model for Solving Delay Problem in Air Traffic Management System." Journal of Computational and Theoretical Nanoscience 17, no. 7 (July 1, 2020): 3160–63. http://dx.doi.org/10.1166/jctn.2020.9154.

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Nowadays, due to the rapid growth of air traffic and airspace congestion flight delays are becoming serious problems. This situation happens due to the demand capacity imbalances in air traffic management system. The deterioration of the expected service and operational costs would be the direct impact of this problem. Network-wide air traffic flow management can be regarded as an effective way to ease demand-capacity imbalances globally and would be able to reduce airspace congestion and flight delays. This paper proposes an integer programming model to solve the problem. The objective function consists of minimizing operational costs and risk costs.
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