Results 21 to 30 of about 318 (178)

An Energetic Eruption With Associated SO 1.707 Micron Emissions at Io's Kanehekili Fluctus and a Brightening Event at Loki Patera Observed by JWST

open access: yesJournal of Geophysical Research: Planets, Volume 128, Issue 8, August 2023., 2023
Abstract We observed Io with the James Webb Space Telescope (JWST) while the satellite was in eclipse, and detected thermal emission from several volcanoes. The data were taken as part of our JWST‐ERS program #1373 on 15 November 2022. Kanehekili Fluctus was exceptionally bright, and Loki Patera had most likely entered a new brightening phase.
Imke de Pater   +26 more
wiley   +1 more source

Optimal Design of Satellite Constellation Korean Peninsula Regions [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2008
Designing satellite constellations providing partial coverage of certain regions becomes more important as small low-altitude satellites receives an increasing attention due to its cost-effectiveness analysis.
Nam-Kyun Kim   +3 more
doaj   +1 more source

Bivariate Infinite Series Solution of Kepler’s Equations

open access: yesMathematics, 2021
A class of bivariate infinite series solutions of the elliptic and hyperbolic Kepler equations is described, adding to the handful of 1-D series that have been found throughout the centuries.
Daniele Tommasini
doaj   +1 more source

Gas-surface interactions modelling influence on satellite aerodynamics and thermosphere mass density

open access: yesJournal of Space Weather and Space Climate, 2021
The satellite acceleration data from the CHAMP, GRACE, GOCE, and Swarm missions provide detailed information on the thermosphere density over the last two decades.
March Günther   +5 more
doaj   +1 more source

Real-Time Orbit Determination for Future Korean Regional Navigation Satellite System [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2016
This paper presents an algorithm for Real-Time Orbit Determination (RTOD) of navigation satellites for the Korean Regional Navigation Satellite System (KRNSS), when the navigation satellites generate ephemeris by themselves in abnormal situations.
Hyungjik Oh   +2 more
doaj   +1 more source

Improved GPS-based Satellite Relative Navigation Using Femtosecond Laser Relative Distance Measurements [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2016
This study developed an approach for improving Carrier-phase Differential Global Positioning System (CDGPS) based realtime satellite relative navigation by applying laser baseline measurement data.
Hyungjik Oh   +4 more
doaj   +1 more source

Implications of cohesive strength in asteroid interiors and surfaces and its measurement

open access: yesProgress in Earth and Planetary Science, 2018
Recent observations and theory have indicated that rubble pile asteroids may have a small, but finite, level of tensile strength, allowing them to spin above their spin deformation limit as defined in Holsapple (Icarus 205:430–442, 2010).
Daniel J. Scheeres, Paul Sánchez
doaj   +1 more source

Computation of Eclipse Time for Low-Earth Orbiting Small Satellites

open access: yesInternational Journal of Aviation, Aeronautics, and Aerospace, 2019
This paper addresses a method for computing eclipse and daylight time for satellites in LEO. Continuous health-monitoring of the satellite is required for the success the mission.
Sumanth R M
doaj   +1 more source

Preliminary Test of Adaptive Neuro-Fuzzy Inference System Controller for Spacecraft Attitude Control [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2012
The problem of spacecraft attitude control is solved using an adaptive neuro-fuzzy inference system (ANFIS). An ANFIS produces a control signal for one of the three axes of a spacecraft’s body frame, so in total three ANFISs are constructed for 3-axis ...
Sung-Woo Kim   +2 more
doaj   +1 more source

Application of Analytic Solution in Relative Motion to Spacecraft Formation Flying in Elliptic Orbit [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2008
The current paper presents application of a new analytic solution in general relative motion to spacecraft formation flying in an elliptic orbit. The calculus of variations is used to analytically find optimal trajectories and controls for the given ...
Hancheol Cho   +2 more
doaj   +1 more source

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