Results 241 to 250 of about 142,311 (289)
Layer-resolved berry curvature and Rashba spin-orbit control of quantum transport in magnetic tunnel junctions. [PDF]
Ghobadi N, Daqiq R, Moradi SAH.
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What has changed in thyroid eye disease in the last five years (2020-2025). [PDF]
Salvi M.
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Spatiotemporal prediction of mining-induced surface subsidence using integrated D-InSAR and boltzmann time function models. [PDF]
Zhou W +5 more
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Quality Control of GFZ Orbit Predictions
D. König, R. Schmidt, Rolf König
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Orbit prediction and Earth shadow modeling for Chandrayaan-2 Orbiter
Astrophysics and Space Science, 2021Chandrayaan-2, India’s second Moon mission, comprised of Orbiter, Lander and Rover modules was launched on July 22, 2019. The Chandrayaan-2 (CH2) Orbiter, which carries eight scientific payloads, is placed into a circular lunar orbit of 100 km altitude with an orbital period of around 120 minutes. After the successful injection of the spacecraft in the
Vineet K. Srivastava +3 more
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Unstable periodic orbits and prediction
Physical Review A, 1991A hierarchical approximation of a generic chaotic attractor can be formulated in terms of unstable periodic orbits. We demonstrate the possibility of extracting the most dominant unstable periodic orbits from a measurement of a time-continuous flow. Since unstable periodic orbits not only represent the static properties of the system but also dominate ...
, Pawelzik, , Schuster
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2018
The OTV fulfills orbital maneuver by selecting appropriate transfer points to save fuels. Usually, before the orbital maneuver, it shall carry out non-powered free sliding in large elliptic orbit for a long time. During such process, due to the longer sliding period, the error of inertial navigation will be accumulated as time elapses.
Xuefeng Li, Chaobing Li
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The OTV fulfills orbital maneuver by selecting appropriate transfer points to save fuels. Usually, before the orbital maneuver, it shall carry out non-powered free sliding in large elliptic orbit for a long time. During such process, due to the longer sliding period, the error of inertial navigation will be accumulated as time elapses.
Xuefeng Li, Chaobing Li
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Nimerical Averaging in Orbit Prediction
AIAA Journal, 1972This paper is a presentation of some useful aspects of a numerical averaging technique that has been applied with considerable success to the orbit prediction problem for artificial satellites. The method has been tested in a variety of situations wherein the satellite is subjected to combinations of perturbations for which adequate analytic theories ...
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