Progress in space weather modeling in an operational environment

Download

index.pdf

Date

2013-01-01

Author

Tsagouri, Ioanna
Belehaki, Anna
Bergeot, Nicolas
Cid, Consuelo
Delouille, Veronique
Egorova, Tatiana
Jakowski, Norbert
Kutiev, Ivan
Mikhailov, Andrei
Nunez, Marlon
Pietrella, Marco
Potapov, Alexander
Qahwaji, Rami
Tulunay, Yurdanur
Velinov, Peter
Viljanen, Ari

Metadata

Show full item record

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Item Usage Stats

188
views

95
downloads

This paper aims at providing an overview of latest advances in space weather modeling in an operational environment in Europe, including both the introduction of new models and improvements to existing codes and algorithms that address the broad range of space weather's prediction requirements from the Sun to the Earth. For each case, we consider the model's input data, the output parameters, products or services, its operational status, and whether it is supported by validation results, in order to build a solid basis for future developments. This work is the output of the Sub Group 1.3 "Improvement of operational models'' of the European Cooperation in Science and Technology (COST) Action ES0803 "Developing Space Weather Products and services in Europe'' and therefore this review focuses on the progress achieved by European research teams involved in the action.

Subject Keywords

Space weather, Modelling, Forecasting, Space environment

URI

https://hdl.handle.net/11511/51672

Journal

JOURNAL OF SPACE WEATHER AND SPACE CLIMATE

DOI

https://doi.org/10.1051/swsc/2013037

Collections

Graduate School of Natural and Applied Sciences, Article

Suggestions

OpenMETU
Core

Numerical analysis of the effects of atmospheric parameters on space launch center safety Yaman, İbrahim; Aksel, Mehmet Haluk; Department of Mechanical Engineering (2016) This thesis study aims at the problem of space launch center safety which is dependent on launch vehicle conceptual design and atmospheric parameters. Selection of the concept at the initial step of the satellite launch vehicle affects the project cost and space launch center safety directly. It is also important to model properties of atmospheric conditions and conduct safety analysis. Successful mission for a launch vehicle depends on providing the total velocity requirement. In this study, launch vehicle...
Global Site Selection for Astronomy AKSAKER, NAZIM; Yerli, Sinan Kaan; Erdogan, M. A.; Kurt, Z.; Kaba, K.; Bayazit, M.; YEŞİLYAPRAK, Cahit (Oxford University Press (OUP), 2020-03-01) A global site selection for astronomy was performed with 1 km spatial resolution (similar to 1 gigapixel in size) using long-term and up-to-date datasets to classify the entire terrestrial surface of the Earth. Satellite instruments are used to get the following datasets of geographical information system (GIS) layers: cloud coverage, digital elevation model, artificial light, precipitable water vapour, aerosol optical depth, wind speed, and land use and land cover. A multi-criteria decision analysis (MCDA)...
Terrain modeling and atmospheric turbulent flow solutions based on meteorological weather forecast data Leblebici, Engin; Tuncer, İsmail Hakkı; Department of Aerospace Engineering (2012) In this study, atmospheric and turbulent flow solutions are obtained using meteorological flowfield and topographical terrain data in high resolution. The terrain topology of interest, which may be obtained in various resolution levels, is accurately modeled using structured or unstructured grids depending on whether high-rise building models are present or not. Meteorological weather prediction software MM5, is used to provide accurate and unsteady boundary conditions for the solution domain. Unsteady turb...
Autonomous spacecraft rendezvous and docking on safe trajectories Büyükkoçak, Ali Tevfik; Tekinalp, Ozan; Department of Aerospace Engineering (2018) In this thesis, rendezvous and docking operation of a pair of low earth orbit spacecraft is addressed. Two different sets of equations for the nonlinear orbital relative motion of spacecraft are derived and simulation codes for this motion are developed. First, Hill-Clohessy-Wiltshire (HCW) equations are used in chaser-target spacecraft configuration with Model Predictive Control (MPC) algorithm including some safety considerations such as debris avoidance, direction of approach constraint and slow impact r...
Atmospheric turbulent flowsolutions coupled with a mesoscale weather prediction model Leblebici, Engin; Ahmet, Gökhan; Tuncer, İsmail Hakkı (2013-01-01) Atmospheric turbulent flow solutions coupled with a mesoscale meteorological weather prediction software are obtained on terrain fitted high resolution computational grids using FLUENT as a CFD tool. The terrain topology of interest, which may be obtained in various resolution levels, is accurately modeled using unstructured grids. The widely used meteorological weather prediction software WRF is used to provide unsteady boundary conditions for the CFD solution domain. Due to difference of mesh structure an...

Citation Formats

I. Tsagouri et al., “Progress in space weather modeling in an operational environment,” JOURNAL OF SPACE WEATHER AND SPACE CLIMATE, pp. 0–0, 2013, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/51672.