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Relevant bibliographies by topics / Cargo flights

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Academic literature on the topic 'Cargo flights'

Author: Grafiati

Published: 4 June 2021

Last updated: 7 February 2022

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Journal articles on the topic "Cargo flights"

1

Peng, Yang, Pu Wang, Xiaolong Zhao, Meilin Chen, Jun Zhang, and Fan Zhang. "A data-driven air cargo redistribution model based on multiple programming." International Journal of Modern Physics B 33, no. 17 (July 10, 2019): 1950176. http://dx.doi.org/10.1142/s0217979219501765.

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Air cargo transportation is an essential mode of cargo transportation. How to distribute air cargo into flights better is an important operational problem. In this paper, air cargo data collected by CAAC (Civil Aviation Administration of China) during the first three months of 2018 are analyzed. We find that the available capacity for cargo transportation shows great variations, and the cargo compartment utilization rates of flights are heterogeneously distributed. Next, a data-driven air cargo redistribution model is developed based on multiple programming (MP). The proposed model can effectively transport high-priority goods and balance cargo compartment utilization rates of flights. In addition, the proposed model framework can provide a new solution to multi-objective or multi-stage optimization problems.

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Siahaan, Juanda. "Penetapam Flow Cargo di Bandara Soekarno Hatta." WARTA ARDHIA 36, no. 4 (December 31, 2010): 302–16. http://dx.doi.org/10.25104/wa.v36i4.93.302-316.

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As a cargo hub airports, at Soekarno Hatta Airport happen every activities of air cargo transport service is very solid, both for domestic and international flights, domestic foreign. For air cargo transport service activities with overseas flight routes, there are two types of service activities that outgoing and incoming cargo export import cargo. Both types of activities are certainly bureaucratic administrative proceess requires that long.As a country that has the potential to increase the capacity of cargo transportation, and has a tremendous opportunity increase economic growth through air freight cargo, then the need for discussion between various parties associated with flow cargo process in Indonesia.

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Sugiyanto, Gito, Purwanto Bekti Santosa, Jajang, Ari Fadli, and Mina Yumei Santi. "Evaluation of hub-spoke airport networks in Sumatra island, Indonesia to increase efficiency of air transportation." MATEC Web of Conferences 195 (2018): 04009. http://dx.doi.org/10.1051/matecconf/201819504009.

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Kualanamu International Airport is the busiest airport in Sumatra. In 2015, it served 8 million passengers and 41.6 thousand tons of goods for international and domestic flights. Hub-spoke networks are optimized when generally having a transport efficiency of at least 49-52% as well as providing air service in a wide geographic area and to many destinations. The aim of this study is to analyse the hub-spoke airport networks based on the Herfindahl-Hirschmann Index (HHI) to increase air transport efficiency in Sumatra Island. This study uses data from cargo production and couple’s flights from 10 airports in Sumatra Island for domestic flight route pairs and 6 airports for international flight route pairs. The results of the study show that route networks in Sumatra Island in existing conditions have not developed with the hub-spokes concept. The HHI analysis, indicates 2 hubs for domestic flights and 1 hub (Kualanamu) for international flights. Kualanamu International Airport and Hang Nadim International Airport were indicated as hub airports in Sumatra Island for domestic flights. The efficiency of air cargo transportation through the system (2 hubs and 8 spokes) results in a transport efficiency at 68.37%, which is still far above the efficient range at 49-52%.

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Virág, László. "Perspectives of air cargo activities in case of Debrecen International Airport." Acta Agraria Debreceniensis, no. 47 (July 18, 2012): 131–34. http://dx.doi.org/10.34101/actaagrar/47/2443.

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The improvement of Debrecen International Airport has been taking place for more than a decade. The goal is to revitalise the domestic and international aviation of regional centres and connect the Debrecen centred economy zone with other industrial and commercial regions. Considering the market segments of the air cargo industry, and sizing up the requirements of the enterprises, we are seeking to answer for what possibilities an air cargo operation has, and scheduled cargo flights, what alternatives the location of a cargo base has. Getting to know the technical background of ground handling, communication, safety, and security, we can state that the airport is able to handle international cargo aircrafts as well. Regarding to the quantity of frights, we find that there is a possibility of two flights per week. There is minor need of handling dangerous or unique parcels. The surrounding area of working zone is an excellent territory for locating and building cargo facilities, and its technical background. In case of continuously increasing traffic it is suggestible to use the territory behind the apron as a first step of the development. As the activity extends the second step could be the improvement of the southern zone just beside the runway. This way primarily thescheduled air cargo flights could appear, then as the traffic of commercial scheduled flights increases simultaneously could grow the amount ofsmall parcel transportation.

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Sahun, Yelyzaveta, Anatoliy Zalevskii, Natalya Chornohor, and Yuliya Sikirda. "Development and visualization of the computer loadıng plannıng model for the cargo aırcraft." Eastern-European Journal of Enterprise Technologies 3, no. 3 (111) (June 30, 2021): 24–31. http://dx.doi.org/10.15587/1729-4061.2021.235629.

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Loading an aircraft is an extremely complex process with many variable aspects that determine the planning of each flight separately. The article is devoted to the development of an algorithm and a computer model for planning the loading of a cargo ramp aircraft in a multi-lag route. The essence of the algorithm consists in a predetermined arrangement of cargo containers relative to the cargo compartment, taking into account the general limitations of the aircraft and the priority of the cargo, which directly affects the planning of loading in a multi-lag route. The use of a visualized computer model created on the basis of the algorithm can reduce the average time of loading operations for a number of direct flights by almost 7 %, and on multi-lag flights by 12 %. Implementation of the model in the activities of an air carrier avoids a situation where certain criteria and restrictions entail sorting «manually» by all indicators, which is very time-consuming in the context of the urgency of servicing the aircraft at the airport. The visualized load planning computer model enables flight planning personnel to make faster decisions and predict additional load on other sections of the route. The successful application of the model to the airline’s operations contributes to the efficiency and safety of ground handling services. This contributes to the intensification of the use of the aircraft fleet by increasing the speed of commercial cargo handling. In the future, the computer model can serve as the basis for a rule-based expert system in order to prevent containers from being overloaded at intermediate sections of the route

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Mrňa, Dominik. "Space flights a new option for intercontinetal travel – solution desing." AEROjournal 16, no. 2 (2020): 19–25. http://dx.doi.org/10.26552/aer.c.2020.2.4.

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This paper describes problem of space flight intercontinental flight with passengers or cargo via suborbital orbits. It describes the necessary monitoring network as well as the operating procedures with connection of flights in airspace and in space itself. Paper takes into account existing models of spacecraft (space vessels) and concept designs to introduce possible solutions to this type of travelling. Last section deals with the issue of ground infrastructure – spaceport, for a given type of transport and focuses on the existing spaceport in USA and presents it as a model for future spaceports around the world.

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Baxter, Glenn, Panarat Srisaeng, and Graham Wild. "The Air Cargo Carrying Potential of The Airbus A350-900XWB and Boeing 787-9 Aircraft on Their Ultra-Long-Haul Flights: A Case Study for Flights from San Francisco to Singapore." Transport and Telecommunication Journal 19, no. 4 (December 1, 2018): 301–14. http://dx.doi.org/10.2478/ttj-2018-0025.

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Abstract The introduction of the Airbus A350-900 (A359) and the Boeing B787-9 (B789) have enabled airlines to operate ultra-long-range services. Using a mixed methods research design, this study has examined the air cargo-carrying potential of Singapore Airlines Airbus A350-900XWB (A359) and United Airlines Boeing B787-9 (789) aircraft on their ultra-long-haul San Francisco to Singapore and the Singapore to San Francisco air routes. The qualitative data was analysed using document analysis, and the air cargo payload was modelled by simulation. The air cargo-carrying potential of the two aircraft types was significantly influenced by enroute weather. In the event of eastbound winds, the Singapore Airlines Airbus A350-900XWB air cargo payload was 16.9 tonnes and the United Airlines Boeing 787-9 was 11.5 tonnes, when these flights had a full passenger payload. In the case of westbound winds with a full passenger payload, the Singapore Airlines Airbus A350-900XWB air cargo payload was 13.1 tonnes and the United Airlines Boeing 787-9 was 7.9 tonnes. When there were no winds on the air routes, the Singapore Airlines Airbus A350-900XWB offered 15.0 tonnes and the United Airline Boeing 787-9 offered 9.7 tonnes of air cargo payload, respectively.

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Mrozowska, Alicja. "ORGANIZATION OF FLIGTHS ON THE DRILLING AND PRODUCTION INSTALLATIONS, IN THE FIELD OF THE SAFETY OF FLIGHT`S PASSANGER." Rocznik Bezpieczeństwa Morskiego XIII (January 24, 2020): 1. http://dx.doi.org/10.5604/01.3001.0013.7505.

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The paper discusses the rules of organizing flights to offshore installations in the wide aspect of safety of passenger and cargo transport by air. The study, analysis the institutions responsible for the safety and organization of air transport, with particular emphasis on the work carry out on the British Shelf and the Baltic Sea. In addition, selected requirements for helicopters, air operators and offshore installations, in particular landing area, equipment and installations readiness to take the helicopter were presented in terms of on board, along with operational procedures for ensuring safety and flight organization.

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Banaszak, David, Dansen Brown, and David Laird. "Antonomous Environmental Definition of C-130 Flap Well Skin Panel." Journal of the IEST 48, no. 1 (September 1, 2005): 50–61. http://dx.doi.org/10.17764/jiet.48.1.pw070l022uu28503.

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Air Force C-130 aircraft require numerous aluminum doubler repairs on the wing flap skin aft of the right-hand outboard engine. These repairs are costly and require riveting. Rivets often provide new areas of stress concentration, which causes new cracks to develop elsewhere. Boeing and the Air Force Research Laboratory (AFRL) are measuring the thermal and strain environment behind the right-hand outboard engine of a North Carolina Air National Guard (NCANG) operational C-130 aircraft (TN 93-1456) for use in design of a damped repair patch to prevent the growth of cracks in skin under the wing flap panel. During June 2003. AFRL engineers and technicians acquired data using an autonomous damage dosimeter during five operational C-130 flights. The damage dosimeter measures structural strains and temperatures on in-service aircraft to diagnose structural conditions that are difficult to analyze, such as acoustics and high cycle fatigue (HCF). The first flight was from Charlotte, North Carolina to Warner Robins Air Force Base (AFB), Georgia and returned to Charlotte. The last four flights were assault flights where the C-130 simulated cargo drops. Pilots logged the altitude and indicated airspeed, engine speed, and flap positions for the first four flights. Flap position settings were compared with dosimeter temperature and root mean square (rms) strain measurements. This paper presents typical third octave plots showing engine speed vibratory frequencies, rms time histories (TH), and correlation data for a flight. This paper also presents typical limited data in TH, probability density function (PDF), power spectral density (PSD), and rain flow formats.

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Veatch, Michael, and Jarrod Goentzel. "Feeding the bottleneck: airport congestion during relief operations." Journal of Humanitarian Logistics and Supply Chain Management 8, no. 4 (December 3, 2018): 430–46. http://dx.doi.org/10.1108/jhlscm-01-2018-0006.

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Purpose Scheduling the airlift of relief supplies into a damaged or small airport during a crisis is complex yet crucial. The volume of cargo and flights can temporarily overwhelm the airport’s capacity and the mix of flights adds complexity. The purpose of this paper is to better characterize airport operations during a crisis, to develop a model that can assess strategies for scheduling flights and to draw implications for decision makers. Design/methodology/approach First, empirical data are analyzed to characterize airport operations. Previously unreported data from the 2010 Haiti earthquake response in the form of a “flight log” are analyzed to provide new insights and parameters. Alternate scheduling strategies are drawn from review of the literature and After Action Reports. Second, a queuing model is developed to understand operations in past crises and predict the impact of alternate scheduling strategies. Empirical data provide the parameters for airport scenarios evaluated. Findings Unloading capacity is seen to be the bottleneck but also to not be fully utilized, suggesting that a more aggressive flight schedule is needed. Scheduling flights is shown to be a tradeoff between volume of aid delivered and flights that must be diverted. The proper mix of aircraft and prioritized divert policies also provide benefits. Finally, it is beneficial, though perhaps counterintuitive, to create a parking buffer upstream from the unloading bottleneck. Originality/value Analysis of previously unreported data from the Haiti earthquake provides new insights regarding airport parking and unloading operations. A new model of airport scheduling for disaster response is proposed. The model differs from other humanitarian airlift models in that it focuses on aircraft parking and unloading. It differs from commercial aircraft scheduling and gate assignment in the objective used.

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Dissertations / Theses on the topic "Cargo flights"

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Lewis, Theresa A. "A comparison of AMC cargo channel flights and alternative commercial air freight carriers." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 1995. http://handle.dtic.mil/100.2/ADA295116.

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Tomanová, Veronika Anna. "Vyhodnocení závislosti HDP na provozních výkonech letecké dopravy." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2015. http://www.nusl.cz/ntk/nusl-232085.

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The diploma thesis describes performance in the area of air transport, based on performance of national economies of two selected neighbouring countries, Czech Republic and Germany, through comparison of their gross domestic product in the selected time period. The operating performance is focused mainly on transportation performance of air transport. First part of the thesis is dealing with interconnection of economy with air transportation. Crucial part of the work contains analysis of development of GDP and analysis of development of transportation performance of both countries. Part of the thesis is also acquisition of passenger-kilometre data derived from fuel consumption and produced emissions of CO2.

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Calvert, N. "Time-of-flight Compton scatter imaging for cargo security." Thesis, University College London (University of London), 2016. http://discovery.ucl.ac.uk/1503664/.

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By measuring the time of flight of scattered x-ray photons, the point of interaction, assuming a single scatter, can be determined, providing a three dimensional image of cargo containers. The present work introduces the technique, and provides experimental and theoretical results to show the feasibility of such a technique. Monte Carlo simulations were performed to investigate the proportion of multiple scatter detected using a proposed experimental setup, and it was found that it accounted for almost 50% of the recorded signal. Monte Carlo simulations of a scintillation detector were provided and used to design the detectors used. Experimental measurements at a picosecond length x-ray source resulted in the reconstruction of scatter position of photons interacting in a 5 cm thick test object to an accuracy of 12 cm full width at half maximum. Preliminary experiments were also performed using a conventional commercially available linear accelerator with a pulse length of 170 ns. Deconvolution techniques were applied to the recorded data to estimate the position of scatter. An analytic single scatter forward model was derived from the radiative transfer equation, discretised and the inverse problem was solved using a number of different methods. The alternating direction method of multipliers was adapted for nonlinear problems and provided image quality that was comparable to the gold standard linear method.

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Leite, Nelson Paiva Oliveira, and Lucas Benedito dos Reis Sousa. "Uncertainty Determination with Monte-Carlo Based Algorithm." International Foundation for Telemetering, 2011. http://hdl.handle.net/10150/595756.

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ITC/USA 2011 Conference Proceedings / The Forty-Seventh Annual International Telemetering Conference and Technical Exhibition / October 24-27, 2011 / Bally's Las Vegas, Las Vegas, Nevada
The measurement result is complete only if it contains the measurand and its units, uncertainty and coverage factor. The uncertainty estimation for the parameters acquired by the FTI is a known process. To execute this task the Institute of Research and Flight Test (IPEV) developed the SALEV© system which is fully compliant with the applicable standards. But the measurement set also includes Derived Parameters. The uncertainty evaluation of these parameters can be solved by cumbersome partial derivates. The search for a simpler solution leads us to a Monte-Carlo based algorithm. The result of using this approach are presented and discussed.

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Cook, Allan B. "Application of neural networks to indirect monitoring of helicopter loads from flight variables." Thesis, This resource online, 1991. http://scholar.lib.vt.edu/theses/available/etd-12052009-020021/.

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Muzic, Raymond Frank Jr. "Monte Carlo analysis of scattered radiation in time-of-flight positron emission tomography." Case Western Reserve University School of Graduate Studies / OhioLINK, 1991. http://rave.ohiolink.edu/etdc/view?acc_num=case1056039087.

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Masinde, Brian. "Birds' Flight Range. : Sensitivity Analysis." Thesis, Linköpings universitet, Institutionen för datavetenskap, 2020. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-166248.

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’Flight’ is a program that uses flight mechanics to estimate the flight range of birds. This program, used by ornithologists, is only available for Windows OS. It requires manual imputation of body measurements and constants (one observation at a time) and this is time-consuming. Therefore, the first task is to implement the methods in R, a programming language that runs on various platforms. The resulting package named flying, has three advantages; first, it can estimate flight range of multiple bird observations, second, it makes it easier to experiment with different settings (e.g. constants) in comparison to Flight and third, it is open-source making contribution relatively easy. Uncertainty and global sen- sitivity analyses are carried out on body measurements separately and with various con- stants. In doing so, the most influential body variables and constants are discovered. This task would have been near impossible to undertake using ’Flight’. A comparison is made amongst the results from a crude partitioning method, generalized additive model, gradi- ent boosting machines and quasi-Monte Carlo method. All of these are based on Sobol’s method for variance decomposition. The results show that fat mass drives the simulations with other inputs playing a secondary role (for example mechanical conversion efficiency and body drag coefficient).

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Simon, Wedlund Mea. "MERCURY In-flight calibration of the PHEBUS UV instrument and Monte Carlo modelling of the hydrogen exosphere." Phd thesis, Université Pierre et Marie Curie - Paris VI, 2011. http://tel.archives-ouvertes.fr/tel-00667491.

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Une caractéristique unique de l'environnement spatial de Mercure est le fort couplage qui existe entre la surface, l'exosphère, la magnétosphère et le vent solaire. Ce système peut être étudié par des méthodes de télédétection embarquées sur les missions spatiales telles que Mariner 10, MESSENGER et bientôt BepiColombo, ainsi que par les observatoires au sol. L'exosphère de Mercure est un milieu complexe avec seulement quelques espèces détectées jusqu'ici, dont l'hydrogène atomique H. H a seulement été détecté une fois par la sonde Mariner 10 en 1974-1975 et représente un traceur de l'interaction entre le vent solaire et la planète Mercure. L'instrument PHEBUS 'a bord de la mission ESA/JAXA BepiColombo vers Mercure est un spectromètre double canal EUV-FUV capable de détecter les émissions les plus faibles, comme H I Lyman-α 'a 121.6 nm. La première partie de cette thèse se concentre sur la modélisation radiométrique et la simulation des performances de PHEBUS. Pour préparer la calibration spectrale en vol et pendant la phase orbitale, un ensemble d'étoiles de référence est déterminé et évalué pour tirer partie au mieux de la résolution et du domaine spectral du détecteur. Des prévisions sur la possibilité de détection des raies d'émission exosphériques sont également données (science performance). Comme PHEBUS est basé sur SPICAV, le spectromètre UV de Venus Express, des techniques semblables de calibration spectrale peuvent être utilisées. Une étude des occultations stellaire de SPICAV est réalisée dans la deuxième partie de cette thèse. Les spectres des étoiles sont extraits, analysés et convolués avec la fonction instrumentale en vue de préparer les futures observations de PHEBUS. Les résultats sont disponibles dans la base de données de calibration du groupe de travail 'a l'ISSI Cross-calibration of past FUV experiments . En parallèle aux nouveaux instruments de grande sensibilité et à haute résolution spectrale, comme PHEBUS, le développement de simulations numériques est nécessaire 'a la compréhension de l'exosphère de Mercure. La troisième partie de cette thèse présente le modèle SPERO, premier modèle auto-cohérent 3D Monte Carlo dédié 'a l'hydrogène exosphérique de Mercure, prenant en compte toutes les sources et les pertes, tels que la désorption thermique, la photoionisation ou la pression de radiation solaire. La désorption thermique est par hypothèse la source dominante d'hydrogène exosphérique. La densité surfacique ainsi que les densités, températures et vitesses exosphériques sont calculées jusqu'à 8 rayons mercuriens. Une étude de sensibilité est effectuée en se basant sur les incertitudes dans les mécanismes de source et de perte, donnant lieu à des asymétries jour/nuit en densité et en température. En utilisant les densités calculées dans un modèle de transfert radiatif, il est possible de comparer les sorties de SPERO avec les données d'émission Lyman-α de Mariner 10, et d'anticiper le retour de données hydrogène grâce 'a l'instrument MASCS embarqué sur la mission MESSENGER de la NASA.

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Wedlund, Mea. "Mercury, in-flight calibration of the PHEBUS UV instrument and Monte Carlo modelling of the hydrogen exosphere." Paris 6, 2011. http://www.theses.fr/2011PA066114.

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L'exosphère de Mercure est complexe avec juste quelques espèces détectées, dont l'hydrogène atomique. Un partie de la thèse présente la modélisation radiométrique de PHEBUS, un spectromètre EUV-FUV capable de détecter les émissions comme Lyman-alpha, à bord de la mission ESA/JAXA BepiColombo. Des prévisions sur la possibilité de détection des raies d'émission exosphériques sont données, grace a un ensemble d'étoiles de référence, déterminé et évalué. L'autre partie de la thèse présente le modèle SPERO, premier modèle 3D Monte Carlo dédié à H exosphérique, prenant en compte toutes les sources/pertes, comme la désorption thermique-la source dominante H, la photoionisation ou la pression de radiation solaire. Les densités, températures et vitesses exosphériques sont calculées. Une étude de sensibilité est effectuée et en utilisant les densités calculées avec transfert radiatif, il est possible de comparer les sorties de SPERO avec les données d'émission Lyman-alpha de Mariner 10.

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Eriksson, Benjamin. "Monte Carlo simulations of a back scatter time-of-flight neutron spectrometer for the purpose of concept testing." Thesis, Uppsala universitet, Tillämpad kärnfysik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-342448.

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The work focuses on Monte Carlo simulations for finding the optimal back scatter time-of-flight spectrometer design for concept testing at the NESSA facility at Uppsala University. The spectrometer consists of two scintillator detectors, D1 (placed in a neutron beam) and D2 (placed in front of D1), at some distance from each other. A fraction of the neutrons that impinge on D1 back scatter into D2 and information on the neutron energy distribution is acquired using the time-of-flight method. For the given constraints on geometry, resolution and efficiency a best resolution was found to be 6.6% with a corresponding efficiency of 1E-4 which gives a sufficient count rate for a neutron generator producing 1E+11 neutrons/s. In order to achieve a minimum of 10 000 counts/h with the same setup a D2 with an area of at least 7 cm^2 is required.

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Books on the topic "Cargo flights"

1

Morelli, Eugene A. Determining the accuracy of aerodynamic model parameters estimated from flight test data. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

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Morelli, Eugene A. Determining the accuracy of aerodynamic model parameters estimated from flight test data. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

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Morelli, Eugene A. Determining the accuracy of aerodynamic model parameters estimated from flight test data. Washington, D.C: American Institute of Aeronautics and Astronautics, 1995.

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San Francisco (Calif.). Office of the Controller. Audits Division. Airport Commission: Concession audit of Gemini Air Cargo, Inc. San Francisco: Office of the Controller, 2004.

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San Francisco (Calif.). Office of the Controller. Audits Division. Airport Commission: Concession audit of Signature Flight Support. San Francisco: Office of the Controller, 2003.

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Izumi, K. H. A conflict analysis of 4D descent strategies in a metered, multiple-arrival route environment. Hampton, Va: NASA Langley Research Center, 1990.

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Izumi, K. H. A conflict analysis of 4D descent strategies in a metered, multiple-arrival route environment. Hampton, Va: NASA Langley Research Center, 1990.

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Cobleigh, Brent R. Development of the X-33 aerodynamic uncertainty model. Edwards, Calif: Dryden Flight Research Center, 1998.

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San Francisco (Calif.). Office of the Controller. Audits Division. Airport Commission: Concession audit of Delta Air Lines, Inc. San Francisco: Office of the Controller, 2003.

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San Francisco (Calif.). Office of the Controller. Audits Division. Airport Commission: Concession audit of Lufthansa German Airlines. San Francisco: Office of the Controller, 2001.

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Book chapters on the topic "Cargo flights"

1

Vlachoudis, V., C. Borcea, S. Buono, P. Cennini, A. Ferrari, Y. Kadi, V. Lacoste, and E. Radermacher. "Monte Carlo Simulation of the Neutron Time-of-Flight Facility at CERN." In Advanced Monte Carlo for Radiation Physics, Particle Transport Simulation and Applications, 1175–80. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-642-18211-2_188.

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Ivaschenko, Anton, Igor Khamits, Petr Skobelev, and Marina Sychova. "Multi-Agent System for Scheduling of Flight Program, Cargo Flow and Resources of International Space Station." In Holonic and Multi-Agent Systems for Manufacturing, 165–74. Berlin, Heidelberg: Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-23181-0_16.

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Jacques, Steven L. "Monte Carlo Modeling of Light Transport in Tissue (Steady State and Time of Flight)." In Optical-Thermal Response of Laser-Irradiated Tissue, 109–44. Dordrecht: Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-8831-4_5.

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Delmas, Rémi, Thomas Loquen, Josep Boada-Bauxell, and Mathieu Carton. "An Evaluation of Monte-Carlo Tree Search for Property Falsification on Hybrid Flight Control Laws." In Numerical Software Verification, 45–59. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-28423-7_3.

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Moore, Kenneth C. "BAGGAGE, CARGO, AND EXEMPT FLIGHTS." In Airport, Aircraft, and Airline Security, 163–76. Elsevier, 1991. http://dx.doi.org/10.1016/b978-0-7506-9019-5.50013-7.

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Marintseva, Kristina, Gennadiy Yun, and Igor Vasilenko. "Delivery of Special Cargoes Using the Unmanned Aerial Vehicles." In Unmanned Aerial Vehicles in Civilian Logistics and Supply Chain Management, 33–63. IGI Global, 2019. http://dx.doi.org/10.4018/978-1-5225-7900-7.ch002.

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This chapter presents the role, functions, and prospects of civil unmanned aerial vehicles development, as well as technical and regulatory barriers to the introduction of unmanned aircraft into special cargo transportation technology. The authors' main idea is that the degree of UAV involvement in freight traffic will continue to grow rapidly as the range of UAV flight and carrying capacity increases, and the air law is liberalized. It is proposed to evaluate the economic efficiency of UAV application and their share in the market for the transportation of urgent and perishable goods using the methodology based on the principles of logistics and mathematical modeling. In the formulated model, the process of special cargoes delivery by unmanned aerial vehicles is integrated into the supply chain by all modes of transport along the set route network, taking into account the requirements formulated by the freight forwarder, carrier, and logistics company.

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Marintseva, Kristina, Gennadiy Yun, and Igor Vasilenko. "Delivery of Special Cargoes Using the Unmanned Aerial Vehicles." In Research Anthology on Reliability and Safety in Aviation Systems, Spacecraft, and Air Transport, 1564–87. IGI Global, 2021. http://dx.doi.org/10.4018/978-1-7998-5357-2.ch066.

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This chapter presents the role, functions, and prospects of civil unmanned aerial vehicles development, as well as technical and regulatory barriers to the introduction of unmanned aircraft into special cargo transportation technology. The authors' main idea is that the degree of UAV involvement in freight traffic will continue to grow rapidly as the range of UAV flight and carrying capacity increases, and the air law is liberalized. It is proposed to evaluate the economic efficiency of UAV application and their share in the market for the transportation of urgent and perishable goods using the methodology based on the principles of logistics and mathematical modeling. In the formulated model, the process of special cargoes delivery by unmanned aerial vehicles is integrated into the supply chain by all modes of transport along the set route network, taking into account the requirements formulated by the freight forwarder, carrier, and logistics company.

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Li, Longbiao. "Risk Assessment of Civil Aircraft during Operation." In Safety and Risk Assessment of Civil Aircraft during Operation. IntechOpen, 2020. http://dx.doi.org/10.5772/intechopen.93557.

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In this chapter, the risk assessment methods for aircraft system, structure, and aeroengine are investigated. For the aircraft system risk assessment, the probability level is divided into probable, improbable, and extremely improbable, and the hazard level of the failure condition is divided into minor, major, and catastrophic. Using Weibull analysis and Bayesian method to analyze the aircraft operation data, the risk level of aircraft system can be determined by combing methods provided in AC 25.1309-1A. For the aircraft structure risk assessment, the probability fracture mechanics approach can be used to determine the structure failure risk based on the data of material properties, environment, inspection, and so on. For the aeroengine risk assessment, the methods for classification of failure risk level, determination of hazard ratio, and calculation of the risk factor and risk per flight are given. The risk assessment process for aeroengine multi-failure modes based on the Monte Carlo simulation is presented to predict the occurrence of the failure and assess the failure risk.

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Conference papers on the topic "Cargo flights"

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Nease, Ardell. "Automated Orbiter options allow cargo-only flights." In Space Programs and Technologies Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-4058.

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Brandes, Tim, Stefano Scarso, Christian Koch, and Stephan Staudacher. "Data-Driven Analysis of Engine Mission Severity Using Non-Dimensional Groups." In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-58673.

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Abstract A numerical experiment of intentionally reduced complexity is used to demonstrate a method to classify flight missions in terms of the operational severity experienced by the engines. In this proof of concept, the general term of severity is limited to the erosion of the core flow compressor blade and vane leading edges. A Monte Carlo simulation of varying operational conditions generates a required database of 10000 flight missions. Each flight is sampled at a rate of 1 Hz. Eleven measurable or synthesizable physical parameters are deemed to be relevant for the problem. They are reduced to seven universal non-dimensional groups which are averaged for each flight. The application of principal component analysis allows a further reduction to three principal components. They are used to run a support-vector machine model in order to classify the flights. A linear kernel function is chosen for the support-vector machine due to its low computation time compared to other functions. The robustness of the classification approach against measurement precision error is evaluated. In addition, a minimum number of flights required for training and a sensible number of severity classes are documented. Furthermore, the importance to train the algorithms on a sufficiently wide range of operations is presented.

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Nicoll, Thomas, and David Mitchell. "ADS-33 Handling Qualities Specification Development for Externally Loaded Cargo/Utility Helicopters." In AIAA Atmospheric Flight Mechanics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-6059.

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Schlenker, Lauren, Andrew J. Sinclair, and Richard Linares. "Angles-Only Orbit Determination Using Hamiltonian Monte Carlo." In 2018 Space Flight Mechanics Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-1975.

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Ghariani, Robin G., and Robert H. Cormier. "Hazardous cargo information management via the flight object." In 2012 Integrated Communications, Navigation and Surveillance Conference (ICNS). IEEE, 2012. http://dx.doi.org/10.1109/icnsurv.2012.6218433.

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Dutta, Gour Gopal, Ankur Singhal, and Ajoy Ghosh. "Estimation of Drag Coefficient from Flight Data of a Cargo Shell." In AIAA Atmospheric Flight Mechanics Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-6149.

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Ilg, Mark, Jonathan Rogers, and Mark Costello. "Projectile Monte-Carlo Trajectory Analysis Using a Graphics Processing Unit." In AIAA Atmospheric Flight Mechanics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-6266.

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Biber, Kasim. "Flight Dynamics Modeling of a Propeller-Driven Cargo Airplane." In 54th AIAA Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-0806.

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Lee, Loo Hay, Huei Chuen Huang, and Peng Huang. "Flight assignment plan for an air cargo inbound terminal." In 2010 Winter Simulation Conference - (WSC 2010). IEEE, 2010. http://dx.doi.org/10.1109/wsc.2010.5678883.

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Laipert, Frank E., and Travis Imken. "A Monte Carlo Approach to Measuring Trajectory Performance Subject to Missed Thrust." In 2018 Space Flight Mechanics Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-0966.

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Reports on the topic "Cargo flights"

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Cicolani, Luigi S., Jeffery Lusardi, Lloyd D. Greaves, Dwight Robinson, Aviv Rosen, and Rueben Raz. Flight Test Results for the Motions and Aerodynamics of a Cargo Container and a Cylindrical Slung Load. Fort Belvoir, VA: Defense Technical Information Center, April 2010. http://dx.doi.org/10.21236/ada517702.

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Roesler, Stefan. Neutron Energy and Time-of-flight Spectra Behind the Lateral Shield of a High Energy Electron Accelerator Beam Dump, Part II: Monte Carlo Simulations. Office of Scientific and Technical Information (OSTI), September 2002. http://dx.doi.org/10.2172/801774.

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