Time-dependent vector constants of motion, symmetries, and orbit equations for the dynamical system <b>r</b>̈=<i>i</i>̂<i>r</i>{[<i>U</i>̈(<i>t</i>)/<i>U</i>(<i>t</i>)]<i>r</i> −[μ/<i>U</i>(<i>t</i>)]<i>r</i>−2} (Q3327764)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Time-dependent vector constants of motion, symmetries, and orbit equations for the dynamical system <b>r</b>̈=<i>i</i>̂<i>r</i>{[<i>U</i>̈(<i>t</i>)/<i>U</i>(<i>t</i>)]<i>r</i> −[μ/<i>U</i>(<i>t</i>)]<i>r</i>−2} |
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Statements
Time-dependent vector constants of motion, symmetries, and orbit equations for the dynamical system <b>r</b>̈=<i>i</i>̂<i>r</i>{[<i>U</i>̈(<i>t</i>)/<i>U</i>(<i>t</i>)]<i>r</i> −[μ/<i>U</i>(<i>t</i>)]<i>r</i>−2} (English)
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1983
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Kepler's problem
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time dependent central force dynamical systems
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vector constants of motion
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procedure for obtaining the orbit equations
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examples
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one-dimensional system
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