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Journal articles on the topic 'Vega Launcher'

Author: Grafiati

Published: 22 February 2023

Last updated: 31 July 2025

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1

Gori, F., M. De Stefanis, W. M. Worek, and W. J. Minkowycz. "Transient thermal analysis of Vega launcher structures." Applied Thermal Engineering 28, no. 17-18 (2008): 2159–66. http://dx.doi.org/10.1016/j.applthermaleng.2007.12.023.

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2

Vandersteen, Jeroen, Samir Bennani, and Christophe Roux. "Robust Rocket Navigation with Sensor Uncertainties: Vega Launcher Application." Journal of Spacecraft and Rockets 55, no. 1 (2018): 153–66. http://dx.doi.org/10.2514/1.a33884.

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3

NAJI, Naji Anees Muqdad, та Adrian-Mihail STOICA. "ℒ1 adaptive controller of VEGA Launcher subject to flexible modes". INCAS BULLETIN 16, № 4 (2024): 81–89. https://doi.org/10.13111/2066-8201.2024.16.4.8.

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Flexible launch vehicle modes contribute to the deterioration of its stability performance. For this reason, their influence must be considered when designing and validating appropriate solutions for its automatic control system. The first three bending modes are the most relevant for control system design and analysis. Next, considerations regarding the elastic modes of the Vega actuator, used in the simulations performed throughout this study, are presented. The IMU (Inertial Measurement Unit) measurements providing attitude angles and angular rates are strongly corrupted by the local elasti

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4

Bianco, Davide, Francesco Adamo, Mattia Barbarino, et al. "Integrated Aero–Vibroacoustics: The Design Verification Process of Vega-C Launcher." Applied Sciences 8, no. 1 (2018): 88. http://dx.doi.org/10.3390/app8010088.

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5

Simplício, Pedro, Samir Bennani, Andrés Marcos, Christophe Roux, and Xavier Lefort. "Structured Singular-Value Analysis of the Vega Launcher in Atmospheric Flight." Journal of Guidance, Control, and Dynamics 39, no. 6 (2016): 1342–55. http://dx.doi.org/10.2514/1.g000335.

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6

Catalano, P., M. Marini, A. Nicolì, and A. Pizzicaroli. "CFD Contribution to the Aerodynamic Data Set of the Vega Launcher." Journal of Spacecraft and Rockets 44, no. 1 (2007): 42–51. http://dx.doi.org/10.2514/1.23534.

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7

Navarro-Tapia, D., A. Marcos, S. Bennani, and C. Roux. "Linear Parameter Varying Control Synthesis for the atmospheric phase VEGA launcher." IFAC-PapersOnLine 51, no. 26 (2018): 68–73. http://dx.doi.org/10.1016/j.ifacol.2018.11.166.

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8

Bianchi, Stefano. "VEGA, the European small launcher: Development status, future perspectives, and applications." Acta Astronautica 63, no. 1-4 (2008): 416–27. http://dx.doi.org/10.1016/j.actaastro.2007.12.058.

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9

Navarro‐Tapia, D., A. Marcos, P. Simplício, S. Bennani, and C. Roux. "Legacy recovery and robust augmentation structured design for the VEGA launcher." International Journal of Robust and Nonlinear Control 29, no. 11 (2019): 3363–88. http://dx.doi.org/10.1002/rnc.4557.

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10

Valli, Monica, Michèle R. Lavagna, and Thomas Panozzo. "Design of a robust control law for the Vega launcher ballistic phase." Acta Astronautica 71 (February 2012): 92–98. http://dx.doi.org/10.1016/j.actaastro.2011.08.002.

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11

Sindoni, G., I. Ciufolini, and F. Battie. "A Monte Carlo Analysis for Collision Risk Assessment on Vega Launcher Payloads and LARES Satellite." Artificial Satellites 51, no. 1 (2016): 45–54. http://dx.doi.org/10.1515/arsa-2016-0004.

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Abstract This work has been developed in the framework of the LARES mission of the Italian Space Agency (ASI). The LARES satellite has been built to test, with high accuracy, the frame–dragging effect predicted by the theory of General Relativity, specifically the Lense–Thirring drag of its node. LARES was the main payload in the qualification flight of the European Space Agency launcher VEGA. A concern arose about the possibility of an impact between the eight secondary payloads among themselves, with LARES and with the last stage of the launcher (AVUM). An impact would have caused failure on

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12

D'Aguanno, Alessandro, Ferry Schrijer, and Bas Van Oudheusden. "Instantaneous Pressure Reconstruction From PIV In Compressible Launcher Environments." Proceedings of the International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics 21 (July 8, 2024): 1–24. http://dx.doi.org/10.55037/lxlaser.21st.173.

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Modern launcher configurations, often characterized by a larger diameter in the payload fairing than the rest of the launch vehicle (hammerhead configuration), face significant challenges during transonic operations, given their susceptibility to flow separation and intense pressure fluctuations. This experimental study aims to reconstruct pressure from PIV under transonic conditions using Taylor's hypothesis. The focus is on the ESA VEGA-E hammerhead launcher model, investigated in the transonic regime at Ma=0.8 and at α=0°. Initially, the methodology of the pressure reconstruction algorithm

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13

Camussi, R., A. Di Marco, C. Stoica, et al. "Wind tunnel measurements of the surface pressure fluctuations on the new VEGA-C space launcher." Aerospace Science and Technology 99 (April 2020): 105772. http://dx.doi.org/10.1016/j.ast.2020.105772.

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14

Haji Jafari, Mohammad, Afshin ValiMohammad, and Mahsa Mahdavi. "Structural Design Modification of a CubeSat Regarding Modal Compatibility for Launching by Vega C Launcher." Journal of Space Science and Technology 16, no. 4 (2023): 41–56. http://dx.doi.org/10.30699/jsst.2023.1439.

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15

Casalino, Lorenzo, Filippo Masseni, and Dario Pastrone. "Viability of an Electrically Driven Pump-Fed Hybrid Rocket for Small Launcher Upper Stages." Aerospace 6, no. 3 (2019): 36. http://dx.doi.org/10.3390/aerospace6030036.

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An electrically driven pump-fed cycle for a hybrid rocket engine is proposed and compared to a simpler gas-pressurized feed system. A liquid-oxygen/paraffin-based fuel hybrid rocket engine which powers the third stage of a Vega-like launcher is considered. Third-stage ignition conditions are assigned, and engine design and payload mass are defined by a proper set of parameters. Uncertainties in the classical regression rate correlation coefficients are taken into account and robust design optimization is carried out with an approach based on an epsilon-constrained evolutionary algorithm. A mis

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16

de Paola, Elisa, Roberto Camussi, Fabio Gasparetti, et al. "Predicting Wall Pressure Fluctuations on Aerospace Launchers Through Machine Learning Approaches." Aerospace 11, no. 12 (2024): 972. http://dx.doi.org/10.3390/aerospace11120972.

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Artificial intelligence (AI) can be used to optimize the prediction of pressure fluctuations over the external surfaces of aerospace launchers and minimize the number of wind tunnel tests. In the present research, various machine learning (ML) techniques capable of predicting the acoustic load were tested and validated. The methods included decision trees, Gaussian Process Regression (GPR), Support Vector Machines (SVMs), artificial neural networks (ANNs), linear regression, and ensemble methods such as bagged and boosted trees. These algorithms were trained using experimental data from an ext

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17

Kovalenko, A. N., V. G. Pereverzev, R. A. Marchan, and Yu V. Blishun. "Experimental verification of the possibility of improving the liquid propelant rocket engine performance for the “Vega” launcher upper stage." VESTNIK of the Samara State Aerospace University, no. 5-1(47) (June 15, 2015): 85. http://dx.doi.org/10.18287/1998-6629-2014-0-5-1(47)-85-95.

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18

Thompson, Joseph William, and William O’Connor. "Wave-Based Attitude Control of Spacecraft with Fuel Sloshing Dynamics." Archive of Mechanical Engineering 63, no. 2 (2016): 263–75. http://dx.doi.org/10.1515/meceng-2016-0015.

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Abstract Wave-Based Control has been previously applied successfully to simple under-actuated flexible mechanical systems. Spacecraft and rockets with structural flexibility and sloshing are examples of such systems but have added difficulties due to non-uniform structure, external disturbing forces and non-ideal actuators and sensors. The aim of this paper is to extend the application of WBC to spacecraft systems, to compare the performance of WBC to other popular controllers and to carry out experimental validation of the designed control laws. A mathematical model is developed for an upper

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19

Marcos, A., V. Mantini, C. Roux, and S. Bennani. "Bridging the gap between linear and nonlinear worst-case analysis: an application case to the atmospheric phase of the VEGA launcher." IFAC Proceedings Volumes 46, no. 19 (2013): 42–47. http://dx.doi.org/10.3182/20130902-5-de-2040.00047.

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20

Stergiou, Vasiliki, Georgios Konstantopoulos, and Costas A. Charitidis. "Carbon Fiber Reinforced Plastics in Space: Life Cycle Assessment towards Improved Sustainability of Space Vehicles." Journal of Composites Science 6, no. 5 (2022): 144. http://dx.doi.org/10.3390/jcs6050144.

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Composite materials, specifically carbon fiber reinforced plastics (CFRPs), are used in various applications such as the automotive, aerospace, and renewable energy industries, thus increasing their global production and volume consumption and creating a subsequent increase in CFRP waste. Especially in space applications and Vega launcher construction, the use of CFRP components to replace metal envisages significant benefits in the use phase by reducing weight and fuel consumption requirements. The current and future waste management and environmental legislation, considering the actual and i

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21

Dalbins, Janis, Kristo Allaje, Hendrik Ehrpais, et al. "Interplanetary Student Nanospacecraft: Development of the LEO Demonstrator ESTCube-2." Aerospace 10, no. 6 (2023): 503. http://dx.doi.org/10.3390/aerospace10060503.

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Nanosatellites have established their importance in low-Earth orbit (LEO), and it is common for student teams to build them for educational and technology demonstration purposes. The next challenge is the technology maturity for deep-space missions. The LEO serves as a relevant environment for maturing the spacecraft design. Here we present the ESTCube-2 mission, which will be launched onboard VEGA-C VV23. The satellite was developed as a technology demonstrator for the future deep-space mission by the Estonian Student Satellite Program. The ultimate vision of the program is to use the electri

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22

Marcos, Andres, Samir Bennani, Christophe Roux, and Monica Valli. "LPV modeling and LFT Uncertainty Identification for Robust Analysis: application to the VEGA Launcher during Atmospheric Phase**This work was funded by ESA-ESTEC Contract No. 4000111052/14/NL/GLC/al within the project ”Analytic Stochastic Time Varying Mu Analysis for the VEGA GNC”." IFAC-PapersOnLine 48, no. 26 (2015): 115–20. http://dx.doi.org/10.1016/j.ifacol.2015.11.123.

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23

Duret, François, and Antonio Fabrizi. "VEGA, a small launch vehicle." Acta Astronautica 44, no. 7-12 (1999): 507–14. http://dx.doi.org/10.1016/s0094-5765(99)00090-9.

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24

Gaudenzi, P., G. Fanchini, and S. Atek. "Feasibility Study of a Vega Launched Geostationary Communication Satellite." Aerotecnica Missili & Spazio 92, no. 3-4 (2013): 101–9. http://dx.doi.org/10.1007/bf03404668.

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25

Escartí-Guillem, Mara S., Sergio Hoyas, and Luis M. Garcia-Raffi. "Deflector shape impact on aero-acoustic noise generation and propagation." Journal of the Acoustical Society of America 152, no. 4 (2022): A222. http://dx.doi.org/10.1121/10.0016076.

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The vibroacoustic loading generated during the launch of space vehicles can cause the failure of electronic and mechanical components. Therefore, the prediction and mitigation of these vibroacoustic levels are crucial to improve the reliability of launchers and payload comfort. Because a properly designed flame deflector has the power to significantly reduce the acoustic pressure level, the aeroacoustics characteristics of diverse types of flame deflectors must be understood. Three different deflector geometries have been analysed: a wedge-type deflector, which is currently used on the VEGA ro

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26

Carreras Lario, Natividad Cristina. "Fernando García de la Vega: un imprescindible en TVE." HUMAN REVIEW. International Humanities Review / Revista Internacional De Humanidades 20, no. 2 (2023): 1–9. https://doi.org/10.37819/revhuman.v20i2.1701.

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Fernando García de la Vega was one of the professionals who launched television in our country. the professionals were true pioneers, inventing formats, imagining content while learning to use the new television technology, and experimenting with the new audiovisual. García de la Vega began doing all kinds of programs, specializing in contests and musicals. he is one of the first and great masters of Spanish television. this work focuses on some of the most emblematic programs that he created, scripted, directed and produced.

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27

Olivero, Mattia, Matteo Ferrai, Piero Pantaleone, et al. "Lumped parameter modelling for the thermal analysis of the launch vehicle Vega C." Aircraft Engineering and Aerospace Technology 90, no. 3 (2018): 542–58. http://dx.doi.org/10.1108/aeat-11-2016-0232.

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Purpose This activity dealt with the thermal analysis of the launch vehicle Vega C through a lumped parameter model. The Vega C is the upgrade of the actual launch vehicle Vega within the Vega Consolidation and Evolution Program, whose objective is to develop a consolidated – hence the C – version of the Vega by 2020. The main aim of the study was verifying the thickness of the external thermal protection of the launch vehicle, such that the structure and equipment temperatures were kept within their operating ranges. Design/methodology/approach The analysis has been performed by means of ESAT

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28

Benmeziane, Karim, and Anne Mione. "Standardization Strategies and Their Impact on Partners' Relationships in Complex Product and Systems." International Journal of IT Standards and Standardization Research 12, no. 2 (2014): 21–37. http://dx.doi.org/10.4018/ijitsr.2014070102.

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In this contribution, the authors investigate the way partners involved in Complex Products and Systems (CoPS) development manage local standards. In particular, this paper analyses how this management impacts the relations between partners through their roles of leader and complementor within platforms. The results are based on a qualitative case study in the launch vehicle segment of the space sector, especially the development of the Ariane 5 and Vega European space launchers. First, the authors find that standards management reveals the firm's position in a platform as a leader or a comple

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29

Pan, Guang, and Jing Wei. "Research on Scene Simulation of Buoy Launched Device System." Applied Mechanics and Materials 433-435 (October 2013): 1921–25. http://dx.doi.org/10.4028/www.scientific.net/amm.433-435.1921.

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For the buoy being launched in the sea, the cost of great number of experiments is very high. It is difficult to get an overall understanding of the process. Aiming at the problems, the visualization of the entire process was realized. Based on Multigen Creator, the three-dimensional models of submarine, buoy, airbag and sleeves were built. Combined simulation program in Vega Prime, the trajectory of the buoy was simulated. In the process of simulation, the viewing angle of the target could be switched for full range of observations. The interaction between users and the simulation system made

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30

HANYOU, Toshio. "Launch opportunity classification of .DELTA.V-EGA and VEGA trajectories to Jupiter." Journal of the Japan Society for Aeronautical and Space Sciences 36, no. 417 (1988): 453–65. http://dx.doi.org/10.2322/jjsass1969.36.453.

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31

Boukid, Fatma, Melisa Lamri, Basharat Nabi Dar, Marta Garron, and Massimo Castellari. "Vegan Alternatives to Processed Cheese and Yogurt Launched in the European Market during 2020: A Nutritional Challenge?" Foods 10, no. 11 (2021): 2782. http://dx.doi.org/10.3390/foods10112782.

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Vegan alternatives to cheese (VAC) and yogurt (VAY) are fast-growing markets in Europe due to the increasing interest in plant-based alternatives to dairy products. This study aimed to take a closer look at the year 2020 and accordingly retrieved the nutritional information of dairy cheese and yogurt and their vegan counterparts for comparison. It was found that VAY (n = 182) provide more energy, total fats, and carbohydrates than dairy yogurt (n = 86), while saturated fatty acids (SFAs), sugars, and salt were not different between the two categories. Compared to dairy products (25.6%), 72.9%

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32

Prokopchuk, A. A., V. A. Shulga, E. V. Strelchenko, et al. "Possible Ways of Modernization of VEGA Launch Vehicle AVUM Stage Main Engine Assembly." Kosmičeskaâ tehnika. Raketnoe vooruženie 2018, no. 2 (2018): 16–24. http://dx.doi.org/10.33136/stma2018.02.016.

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33

Anish B. Krishnan and Dineshsingh G. Thakur. "Evaluation of ‘Design for Assembly’ Performance of Undercut Finocyl Grain Casting Mandrels." Defence Science Journal 75, no. 2 (2025): 224–35. https://doi.org/10.14429/20257.

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Advanced space launch vehicles that employ solid rocket boosters are found to use undercut finocyl-shaped propellant grains. The undercut features, however, cannot be easily manufactured using conventional methods of casting propellant around rigid monolith mandrels or by machining the fin slots. To solve the problem, many non-rigid type mandrels were experimented with without wide acceptance due to functional, performance, or safety issues. Alternatively, in recent times, a few types of rigid undercut finocyl grain mandrels have been developed by different space agencies. While each claims su

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Anish B. Krishnan and Dineshsingh G. Thakur. "Evaluation of ‘Design for Assembly’ Performance of Undercut Finocyl Grain Casting Mandrels." Defence Science Journal 75, no. 2 (2025): 224–35. https://doi.org/10.14429/dsj.20257.

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Advanced space launch vehicles that employ solid rocket boosters are found to use undercut finocyl-shaped propellant grains. The undercut features, however, cannot be easily manufactured using conventional methods of casting propellant around rigid monolith mandrels or by machining the fin slots. To solve the problem, many non-rigid type mandrels were experimented with without wide acceptance due to functional, performance, or safety issues. Alternatively, in recent times, a few types of rigid undercut finocyl grain mandrels have been developed by different space agencies. While each claims su

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35

Kresák, Ĺ., J. Rahe, M. F. A’Hearn, et al. "Commission 15; Physical Study of Comets, Minor Planets and Meteorites." Transactions of the International Astronomical Union 20, no. 1 (1988): 143–66. http://dx.doi.org/10.1017/s0251107x00007100.

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The period covered by this report, 1984 July to 1987 June, was of extraordinary importance for the progress of cometary physics. For the first time in the history, special space probes were launched to comets. Vega 1, Vega 2 and Giotto encountered P/Halley, providing us with the first close-up pictures of a cometary nucleus, its surface features, and with the first in situ measurements of the matter escaping from it. ICE, Suisei and Sakigake carried out measurements relevant to P/Giacobini-Zinner and P/Halley in interplanetary space. Unprecedented worldwide campaigns of ground-based observatio

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36

Llana, David Sánchez de la, Samir Bennani, Irene Cruciani, and Joaquín Aranda. "H-Infinity control of the VEGA Launch Vehicle first stage in presence of roll." IFAC Proceedings Volumes 46, no. 19 (2013): 54–59. http://dx.doi.org/10.3182/20130902-5-de-2040.00039.

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37

Yatskiv, Ya S. "FROM THE HISTORY OF SPACE RESEARCH IN UKRAINE. 2. ІNTERNATIONAL COOPERATION IN PEACEFUL SPACE RESEARCH AND EXPLORATION (1957—1987)". Kosmìčna nauka ì tehnologìâ 29, № 2 (2023): 97–111. http://dx.doi.org/10.15407/knit2023.02.097.

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The article covers a special period of time, from the epochal event of 1957, the launch of the first artificial Earth satellite in the USSR, to the last most successful space project «Vega», carried out under the «Intercosmos» program in 1986. The problems of international cooperation in space exploration and development are highlighted. Information about other space projects of this period and the memories of eyewitnesses of these events are given

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38

Gasparre, Nicola, Marina Mefleh, and Fatma Boukid. "Nutritional Facts and Health/Nutrition Claims of Commercial Plant-Based Infant Foods: Where Do We Stand?" Plants 11, no. 19 (2022): 2531. http://dx.doi.org/10.3390/plants11192531.

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One of the current drivers of the infant food market is the rising demand for vegan products, and thus accurate knowledge of their nutritional composition is required to guide parents and health professionals. Thus, this study aimed to assess the nutritional composition of commercial plant-based infant foods, in addition to analyzing their health/nutrition claims. A selection of infant products launched in the global market (2017–2021) were classified into eight types and each type was divided into vegan and vegetarian products. Based on the ingredients list, cereals, seeds, pseudocereals and/

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39

NAJI, Naji Anees Muqdad, and Adrian STOICA. "L1 adaptive control design for the rigid body launch vehicle." INCAS BULLETIN 15, no. 4 (2023): 187–97. http://dx.doi.org/10.13111/2066-8201.2023.15.4.16.

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This paper investigates the use of an L1-adaptive controller to improve the performance of the Vega launch vehicle because the classical controller does not guarantee stability and tracking of the system in the transient. The L1-AC ensures uniformly bounded transient and steady-state tracking for both systems’ signals, input, and output. In this paper, we used the equations of the adaptation and the L1-norm with two filters, the first one is first-order order and the second filter is third-order, we used the large adaptive gain with the first filter, also used the low adaptive gain with the se

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40

Stankov, Nikolay. "Vera Olivová: Historian and Time." Central-European Studies 6 (2023): 129–60. http://dx.doi.org/10.31168/2619-0877.2023.6.6.

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The author of the article investigates the main stages of scientific activity of the famous Czech professor of history at Charles University in Prague Vera Olivová (1926–2015). This paper is based on the analysis of her publications. In the 1950s and 1960s Vera Olivová published a fundamental monograph on Czechoslovak-Soviet relations from 1918 to 1922 with a large appendix of documents, as well as a series of articles on the relations of the Czechoslovak Republic with neighbouring countries — Germany, Austria, Poland, and Hungary. Despite the fact that they were written in line with the Marxi

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Wordsworth, Saul, and Tom Stone. "Power Player." Industrial Vehicle Technology International 28, no. 1 (2020): 54–58. http://dx.doi.org/10.12968/s1471-115x(23)70479-0.

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THE STAGE IS SET AT CONEXPO IN LAS VEGAS FOR THE NORTH AMERICAN LAUNCH OF THE LARGEST EXCAVATOR IN VOLVO CE'S RANGE. AS THE EC950F ROLLS INTO TOWN, WE GET THE FULL LOWDOWN ON ITS IMPRESSIVE EFFICIENCY LEVELS AND GROUNDBREAKING FEATURES

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42

Carril, Lucia, Marie Naigeon, Cécile Dalban, et al. "The impact of baseline peripheral cytokines on survival in metastatic clear cell renal cell carcinoma (RCC) treated with nivolumab: NIVOREN GETUG-AFU 26 Translational study." Journal of Clinical Oncology 40, no. 6_suppl (2022): 379. http://dx.doi.org/10.1200/jco.2022.40.6_suppl.379.

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379 Background: The NIVOREN GETUG-AFU 26 study reported safety and efficacy of nivolumab in patients with RCC in a “real world setting”. A translational research program was launched to quantify baseline cytokine levels and correlate them with outcomes to nivolumab. Methods: Extreme responder patients (pts) treated with nivolumab as part of the phase II NIVOREN GETUG-AFU 26 were included in this TRAINING cohort. A panel of 14 different plasma cytokines and proteins (VEGF, VCAM-1, IL-6, IL-7, IL-8, IL-10, APRIL, BAFF, 4-1BB, BCA, SDF-1, MDC, IFN-gamma and TNF-alpha) were quantified for each pla

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43

NAJI, Naji Anees Muqdad, and Adrian STOICA. "Design of a robust controller for the VEGA TVC using the L1-Adaptive Control." INCAS BULLETIN 15, no. 4 (2023): 175–85. http://dx.doi.org/10.13111/2066-8201.2023.15.4.15.

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The purpose of this study is to Design of a robust controller for the VEGA TVC using the L1-Adaptive Control. The performance of the system with an L1 adaptive controller has been compared with that of a classical controller. The L1 adaptive controller optimization is an efficient as well as an effective approach for the design of a robust controller. The L1 adaptive controller ensures the robustness of the system against uncertainties, noise, and disturbances[10]. In a launch vehicle parameters like mass, thrust, and aerodynamic properties are time-varying. Due to the time-varying nature of t

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44

Čiamporová-Zaťovičová, Zuzana, Patrik Macko, Michaela Šamulková, Ondrej Vargovčík, Jana Bozáňová, and Jr Fedor Čiampor. "AquaBOL.SK - how far have we come with the Slovak reference barcode database since DNAqua-Net was launched?" ARPHA Conference Abstracts 4 (March 4, 2021): e64939. https://doi.org/10.3897/aca.4.e64939.

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Essential for implementation of molecular tools in bioassessments are comprehensive databases with high-quality reference DNA sequence data. A recent survey arising from the DNAqua-Net EU COST Action WG1 has revealed significant gaps in the barcode reference data of aquatic biota both on a taxonomic and a geographical level (Weigand 2019). Although reference barcode libraries of all main freshwater groups are continuously improved through a number of national DNA-barcoding campaigns, still little data is available from Central and Eastern Europe.In Slovakia, the barcode coverage of the aquatic

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45

Asakage, Masaki, Hidetaka Noma, Kanako Yasuda, Hiroshi Goto, and Masahiko Shimura. "Dynamics of Inflammatory Factors in Aqueous Humor During Brolucizumab Treatment for Age-Related Macular Degenerations: A Case Series." Medicina 61, no. 3 (2025): 372. https://doi.org/10.3390/medicina61030372.

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Anti-vascular endothelial growth factor (VEGF) treatment with intravitreal brolucizumab (IVBr) was launched as a novel treatment for neovascular age-related macular degeneration (AMD), but the incidence of intraocular inflammation (IOI) as a specific adverse effect of brolucizumab has been reported. We evaluated the dynamics of inflammatory factors in AMD in patients with or without IOI before and after anti-VEGF treatment with IVBr. We describe three patients who did not develop inflammation after three consecutive administrations of IVBr and three in whom inflammation occurred after the firs

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Proulx, Mikhel. "Vera Frenkel’s String Games: Improvisations for Inter-City Video." Virtual Creativity 13, no. 2 (2023): 123–30. http://dx.doi.org/10.1386/vcr_00079_1.

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In the autumn of 1974, the Canadian artist Vera Frenkel staged String Games: Improvisations for Inter-City Video. Two groups of participants – five each in Toronto and Montreal – engaged in a remote version of the classic string game cat’s cradle. String Games is the first piece of telematic art. However, art historical attention to the artwork has been insufficient. String Games emerged from a watershed moment for network technologies, specifically within a context of telecommunications development in the Canadian nation state. Telecommunications-based art has a long legacy in Canada, the cou

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Porras-Hermoso, Angel, Javier Cubas, and Santiago Pindado. "On the satellite attitude determination using simple environmental models and sensor data." Journal of Physics: Conference Series 2090, no. 1 (2021): 012116. http://dx.doi.org/10.1088/1742-6596/2090/1/012116.

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Abstract Attitude determination represents a fundamental task for most of the spacecrafts. It relies on three basic aspects: 1) sensors selection, 2) relevant environmental conditions estimation, and 3) algorithms that relate the sensor measurements to the expected conditions in the reference frame. Each one has its own impact on the accuracy that the system can achieve. Besides, two factors stand out above the others in terms of accuracy: 1) sensor quality (calibration, range, etc), and 2) precision of the environmental models. The computation of the satellite attitude needs at least two inde

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Padgett, Deborah L. "SpS1-Preparing for the harvest from large infrared surveys." Proceedings of the International Astronomical Union 5, H15 (2009): 510–11. http://dx.doi.org/10.1017/s1743921310010422.

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During the past decade, there has been a revolution in the availability of multi-wavelength astronomical surveys. From the Sloan Digital Sky Survey (SDSS) to the NRAO VLA Sky Survey (NVSS), astronomical research based on publicly accessible datasets is becoming standard practice in the community. Beginning with the Infrared Astronomical Satellite (IRAS) mission, infrared surveys have played a critical role in stellar astronomy by identifying cool and dusty stars worthy of spectroscopic characterization. IRAS' four photometric bands at 12, 25, 60, and 100 μm were ideal for detecting dusty circu

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Amati, Lorenzo, Riccardo Campana, Yuri Evangelista, et al. "GAME: GRB and All-sky Monitor Experiment." International Journal of Modern Physics D 23, no. 06 (2014): 1430010. http://dx.doi.org/10.1142/s0218271814300109.

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We describe the GRB and all-sky monitor experiment (GAME) mission submitted by a large international collaboration (Italy, Germany, Czech Republic, Slovenia, Brazil) in response to the 2012 ESA call for a small mission opportunity for a launch in 2017 and presently under further investigation for subsequent opportunities. The general scientific objective is to perform measurements of key importance for GRB science and to provide the wide astrophysical community of an advanced X-ray all-sky monitoring system. The proposed payload was based on silicon drift detectors (~1–50 keV), CdZnTe (CZT) de

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Likhvantseva, V. G., O. A. Anurova, S. E. Astakhova, M. V. Vereshchagina, V. E. Ovanesyan, and E. V. Stepanova. "Expression of Vascular Endothelial Growth Factor in Uveal Melanoma." Ophthalmology in Russia 18, no. 4 (2021): 914–21. http://dx.doi.org/10.18008/1816-5095-2021-4-914-921.

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A prerequisite for the growth, progression and metastasis of malignant tumors of any localization is the development of its own vascular network. Newly formed vessels not only nourish the primary tumor, but also create conditions for the spread of tumor cells through the circulatory system and the formation of distant metastases. Angiogenesis is able to launch a small population of tumors from 100–300 cells that have accumulated genetic aberrations and have begun to express proangigenic molecules. The phenomenon is known as “transformation of tumor cells into angiogenic phenotype”. A tumor wit

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