Thermosphere and satellite drag
Accurate forecasts of thermosphere densities, realistic calculation of aerodynamic drag, and propagation of the uncertainty on the predicted orbit positions are required for conjunction analysis and collision avoidance decision making. The main focus of the Committee on Space Research (COSPAR) International Space Weather Action Teams (ISWAT) involved ...
Sean Bruinsma +2 more
exaly +5 more sources
De-Orbit Maneuver Demonstration Results of Micro-Satellite ALE-1 with a Separable Drag Sail
ALE-1, a micro-satellite created for the demonstration of artificial shooting stars, required orbital descent before mission execution due to safety aspects in orbit.
Kohei Takeda +2 more
exaly +3 more sources
Drag-free and attitude control for the GOCE satellite [PDF]
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Enrico Canuto
exaly +3 more sources
Satellite Orbital Drag During Magnetic Storms [PDF]
AbstractWe investigate satellite orbital drag effects at low‐Earth orbit associated with thermosphere heating during magnetic storms caused by coronal mass ejections. CHAllenge Mini‐satellite Payload (CHAMP) and Gravity Recovery And Climate Experiment (GRACE) neutral density data are used to compute orbital drag.
Denny M Oliveira, E Zesta
exaly +5 more sources
Generative AI for Bayesian Computation [PDF]
Generative Bayesian Computation (GBC) provides a simulation-based approach to Bayesian inference. A Quantile Neural Network (QNN) is trained to map samples from a base distribution to the posterior distribution.
Nick Polson, Vadim Sokolov
doaj +2 more sources
Atmospheric drag effects on modelled low Earth orbit (LEO) satellites during the July 2000 Bastille Day event in contrast to an interval of geomagnetically quiet conditions [PDF]
In this work, we simulated the atmospheric drag effect on two model SmallSats (small satellites) in low Earth orbit (LEO) with different ballistic coefficients during 1-month intervals of solar–geomagnetic quiet and perturbed conditions. The goal of this
V. U. J. Nwankwo +10 more
doaj +1 more source
Aerodynamic Drag Characteristics of Ultra-Low Orbit Satellites
Taking the 180~300 km ultra-low orbit satellite as the research object, the aerodynamic drag characteristics of the typical shapes were studied by using the direct simulation Monte Carlo (DSMC) method in the free molecular flow simulation method, which ...
WANG Xiaoliang, YAO Xiaosong, GAO Shuang, LIU Guohua
doaj +1 more source
Drag Sail Conceptual Design for Satellite Orbit Reduction in Low Earth Orbit [PDF]
The main purpose of this paper is to provide a regular design process of drag sail for deorbiting a satellite in LEO orbit concerning the mission requirements. In this regard, the design requirements and manufacturing considerations of the drag sail have
Ali Kasiri +2 more
doaj +1 more source
ON THE CHARACTER OF AN ARTIFICIAL SATELLITE DRAG UNDER VARIOUS STATES OF SOLAR AND GEOMAGNETIC ACTIVITY [PDF]
Purpose: The artificial satellites drag in the atmosphere remains an urgent problem to date. In this work, the artificial satellites data are used in order to study the atmosphere state under various manifestations of solar and geomagnetic activity.
V. H. Komendant
doaj +1 more source
Drag Effect of Kompsat-1 During Strong Solar and Geomagnetic Activity [PDF]
In this paper, we analyze the orbital variation of the KOrea Multi-Purpose SATellite-1(KOMPSAT-1) in a strong space environment due to satellite drag by solar and geomagnetic activities.
J. Park +7 more
doaj +1 more source

