Lagrange equations for the failure orbits elements
Result description
The paper includes a brief description of the results of the problem of the Lagrange planetary equations for the perturbation paths of the Kepler's elements. The perturbation function describes the deviation of the real orbit and the Kepler's orbit. Important part of the paper is to present the geometric interpretation of the derivations of the functions of the body mass.
Keywords
The result's identifiers
Result code in IS VaVaI
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Lagrange equations for the failure orbits elements
Original language description
The paper includes a brief description of the results of the problem of the Lagrange planetary equations for the perturbation paths of the Kepler's elements. The perturbation function describes the deviation of the real orbit and the Kepler's orbit. Important part of the paper is to present the geometric interpretation of the derivations of the functions of the body mass.
Czech name
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Czech description
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Classification
Type
O - Miscellaneous
CEP classification
BN - Astronomy and celestial mechanics, astrophysics
OECD FORD branch
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Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2011
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Basic information
Result type
O - Miscellaneous
CEP
BN - Astronomy and celestial mechanics, astrophysics
Year of implementation
2011