Results 1 to 10 of about 54,135 (313)

NORAD TLE Conversion from Osculating Orbital Element [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2002
The NORAD type Two Line Element (TLE) was obtained from the osculating orbital elements by an iterative approximation procedure. The mathematical model was presented and computer program was developed for the conversion.
Byoung-Sun Lee
doaj   +3 more sources

Primary Orbital Teratoma With Congenital Anophthalmia in a Neonate: A Rare Case With Histopathological and Radiological Correlation [PDF]

open access: yesCase Reports in Ophthalmological Medicine
This case report describes a rare instance of primary orbital teratoma with anophthalmia in a neonate. A 6-day-old female presented with a congenital right orbital swelling and absence of visible ocular structures. MRI revealed a large, well-vascularized
Dejan M. Rašić   +2 more
doaj   +2 more sources

Solar Radiation Pressure Effects on the Orbital Elements of Artificial Earth Satellite

open access: yesTikrit Journal of Pure Science, 2023
The solar radiation pressure is one of the non-conservative force perturbation effects on earth satellite. A method presented to calculate the effect of radiation pressure on orbital elements for different altitude of satellites, the necessary ...
Ahmed K. Izzet
doaj   +1 more source

Neural Network based Fault Tolerant LQR Control for Orbital Maneuvering in LEO Satellites using Hall Effect Thrusters [PDF]

open access: yesAUT Journal of Modeling and Simulation, 2023
This paper develops a neural network-based fault tolerant LQR control for orbital maneuvering of satellites in low altitude orbit that are subjected to disturbances like earth gravity, atmospheric drag, third body, and solar radiation.
Elham Jahanbazi   +2 more
doaj   +1 more source

Improving the Method of Satellite Station Keeping in Geostationary Orbit with Considerations of fuel Consumption Restrictions [PDF]

open access: yesعلوم، فناوری و کاربردهای فضایی, 2022
Due to the unique characteristics of the geostationary orbit and the importance of establishing a satellite in this flying corridor، it is necessary to investigate the effect of environmental disturbances on the orbital elements and to maintain the ...
Hossein Maghsoudi Dehaghani   +3 more
doaj   +1 more source

Observations of the Rigollet Comet from Korea and Japan [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2014
Since Rigollet first discovered a comet in 1939, many follow-up observations have been made, particularly in Europe. It is now known that the Rigollet comet is identical with the one observed by Herschel in 1788, and thus it is now called 35P/1939 O1 ...
Ki-Won Lee   +3 more
doaj   +1 more source

Correlations of Orbital Elements for Visual Double Stars [PDF]

open access: yesSerbian Astronomical Journal, 2010
In this paper, the authors examine the dependence of correlation coefficients of orbital elements on the length of the orbital arc covered by measurements, on measurements of different accuracies, and on the number of measurements.
Milic, I. S., Cvetkovic, Z.
doaj   +3 more sources

Necessary condition for temporary asteroid capture

open access: yesOpen Astronomy, 2023
Asteroid capture holds great significance in understanding the origins of asteroids, the source of life, and the exploration of planetary mineral resources.
Bao Changchun, Li Zhijie, Wang Xianyu
doaj   +1 more source

The Comparison of the Classical Keplerian Orbit Elements, Non-Singular Orbital Elements (Equinoctial Elements), and the Cartesian State Variables in Lagrange Planetary Equations with J2 Perturbation: Part I [PDF]

open access: yesJournal of Astronomy and Space Sciences, 2011
Two semi-analytic solutions for a perturbed two-body problem known as Lagrange planetary equations (LPE) were compared to a numerical integration of the equation of motion with same perturbation force.
Jung Hyun Jo   +3 more
doaj   +1 more source

Approximations for Secular Variation Maxima of Classical Orbital Elements under Low Thrust

open access: yesMathematics, 2023
The reachability assessment of low-thrust spacecraft is of great significance for orbital transfer, because it can give a priori criteria for the challenging low-thrust trajectory design and optimization.
Zhaowei Wang, Lin Cheng, Fanghua Jiang
doaj   +1 more source

Home - About - Disclaimer - Privacy