Abstract

Space weather driven atmospheric density variations affect low Earth orbit (LEO) satellites during all phases of their operational lifetime. Rocket launches, re-entry events and space debris are also similarly affected. A better understanding of space weather processes and their impact on atmospheric density is thus critical for satellite operations as well as for safety issues. The Horizon 2020 project Space Weather Atmosphere Model and Indices (SWAMI) project, which started in January 2018, aims to enhance this understanding by:Developing improved neutral atmosphere and thermosphere models, and combining these models to produce a new whole atmosphere model.Developing new geomagnetic activity indices with higher time cadence to enable better representation of thermospheric variability in the models, and improving the forecast of these indices.The project stands out by providing an integrated approach to the satellite neutral environment, in which the main space weather drivers are addressed together with model improvement. The outcomes of SWAMI will provide a pathway to improved space weather services as the project will not only address the science issues, but also the transition of models into operational services.The project aims to develop a unique new whole atmosphere model, by extending and blending the Unified Model (UM), which is the Met Office weather and climate model, and the Drag Temperature Model (DTM), which is a semi-empirical model which covers the 120–1500 km altitude range. A user-focused operational tool for satellite applications shall be developed based on this. In addition, improved geomagnetic indices shall be developed and shall be used in the UM and DTM for enhanced nowcast and forecast capability.In this paper, we report on progress with SWAMI to date. The UM has been extended from its original upper boundary of 85 km to run stably and accurately with a 135 km lid. Developments to the UM radiation scheme to enable accurate performance in the mesosphere and lower thermosphere are described. These include addition of non-local thermodynamic equilibrium effects and extension to include the far ultraviolet and extreme ultraviolet. DTM has been re-developed using a more accurate neutral density observation database than has been used in the past. In addition, we describe an algorithm to develop a new version of DTM driven by geomagnetic indices with a 60 minute cadence (denoted Hp60) rather than 3-hourlyKpindices (and corresponding ap indices). The development of the Hp60 index, and the Hp30 and Hp90 indices, which are similar to Hp60 but with 30 minute and 90 minute cadences, respectively, is described, as is the development and testing of neural network and other machine learning methods applied to the forecast of geomagnetic indices.

Highlights

  • Precise knowledge of the location and motion of space objects is important, and this importance is rapidly increasing with the advent of large constellations (e.g., National Academies of Sciences, Engineering, and Medicine, 2016; Muelhaupt et al, 2019)

  • We report on progress with Space Weather Atmosphere Model and Indices (SWAMI) to date

  • It is currently used with an upper boundary near 85 km altitude and the aim in this project is to extend its upper boundary to around 170 km altitude to enable coupling with the Drag Temperature Model (DTM), which has a lower boundary at 120 km

Read more

Summary

Introduction

Precise knowledge of the location and motion of space objects is important, and this importance is rapidly increasing with the advent of large constellations (e.g., National Academies of Sciences, Engineering, and Medicine, 2016; Muelhaupt et al, 2019). MCM is an innovative, user-focused tool for use by satellite operators, launch service providers, satellite re-entry analysts as well as space weather scientists It shall benefit the entire user community that requires knowledge of the mean state of the atmosphere and its variability as a function of location and time from the surface up to the top of the thermosphere. MODELS: To develop MOWA (covering the 0–1500 km altitude range), and an operational tool for satellite re-entry and launch applications (MCM) based on MOWA Both models shall provide estimates of both climatology and space weather variability. DRIVERS: To provide nowcasts and forecasts of the new high cadence Hp geomagnetic indices, to be used in the UM and DTM These products are useful for a wide range of space weather services that rely on rapid geomagnetic activity specification.

Concept and methodology
Thermospheric modelling
DTM development and database
DTM algorithm
Model assessments
Extended UM
Initial UM runs and the nudging scheme
The NLTE radiation scheme
Index nowcasting and forecasting
Design of MCM
Requirements for operational application
Findings
Conclusions
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call