Results 1 to 10 of about 173,397,284 (199)
Syndrome spectrums of error orbits in RS-codes
This article is devoted to the research of the properties of syndromes of errors in Reed-Solomon codes. RS-codes are built on non-binary alphabets. So, unlike BCH-codes, RS-codes contain an extremely large variety of correctable errors.
V. A. Lipnitski, S. I. Semyonov
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Error correction by Reed–Solomon codes using its automorphisms
The article explores the syndrome invariants of АГ-group of automorphisms of Reed–Solomon codes (RS-codes) that are a joint group of affine and cyclic permutations. The found real invariants are a set of norms of N Г-orbits that make up one or another АГ-
V. A. Lipnitsky, S. I. Semyonov
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Gradient estimation using configurations of two or three spacecraft [PDF]
The forthcoming three-satellite mission Swarm will allow us to investigate plasma processes and phenomena in the upper ionosphere from an in-situ multi-spacecraft perspective.
J. Vogt +4 more
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The automorphisms and error orbits of Reed – Solomon codes
The purpose of this work with its results presented in the article was to develop and transfer to the class of Reed – Solomon codes (RS-codes) the basic provisions of the theory of syndrome norms (TNS), previously developed for the noise-resistant coding
S. I. Semyonov, V. A. Lipnitsky
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PROPERTIES OF GROUPS G OF DOUBLE ERRORS AND ITS INVARIANTS IN BCH CODES
The goal of the work is the further extending the scope of application of code automorthism in methods and algorithms of error correction by these codes. The effectiveness of such approach was demonstrated by norm of syndrome theory that was developed by
V. A. Lipnitskij, A. V. Serada
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Optical satellite products are available at different processing levels. Of these products, terrain corrected (i.e., orthorectified) products are the ones mostly used for glacier displacement estimation. For terrain correction, a digital elevation model (
Bas Altena, Andreas Kääb
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Evolutionary Approach to Lambert’s Problem for Non-Keplerian Spacecraft Trajectories
In this paper, we use differential evolution (DE), with best-evolved results refined using a Nelder–Mead optimization, to solve boundary-value complex problems in orbital mechanics relevant to low Earth orbits (LEO).
David W. Hinckley, Darren L. Hitt
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Non-Cooperative Target Ranging Based on High-Orbit Single-Star Temporal–Spatial Characteristics
A visible light camera payload with star-sensitive functionality was installed to measure the distance between a non-cooperative target satellite and a high-orbit satellite. The rotation matrix was used to calculate the pointing vector from the center of
Derui Zhang, Hao Wang, Qing Zhao
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Lunar navigation systems are being developed to support sustained surface operations, but their early deployment phase may involve limited satellite visibility and degraded accuracy in orbit and clock determination compared with terrestrial global ...
Rion Sobukawa, Takuji Ebinuma
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Measuring. Monitoring. Management. Control
Background. The task of preventing orbital incidents requires monitoring the occupancy of the working and intermediate orbits of multi-satellite space systems with high-precision determination of the current navigation parameters of each observed ...
S.V. Logunov +3 more
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