File:Comparison of Eccentricity.gif: Difference between revisions
imported>Dan Nessett (uploaded a new version of "Image:Comparison of Eccentricity.gif": {{Image_Details |description = Animated Gif |author = |copyright = |source = |date-created = |pub-country = |notes = |versions = }}) |
imported>Dan Nessett (uploaded a new version of "Image:Comparison of Eccentricity.gif": Reverted to version as of 10:24, 24 March 2010) |
(No difference)
| |
Revision as of 17:25, 17 February 2011
Summary
| Title / Description
|
Two orbits with otherwise identical Orbital elements differ in eccentricity |
|---|---|
| Author(s)
|
Garry R. Osgood |
| Copyright holder
|
Garry R. Osgood See below for license/re-use information. |
| Source
|
Wikimedia Commons |
| Date created
|
31 August 2007 |
| Country of first publication
|
Unknown |
| Notes
|
(This animated gif has been replaced with its first frame, since as of April, 2010, animated gifs cause problems with the wiki software). Two orbiting bodies have orbital elements that differ only in eccentricity. They are each independent two-body systems overlaid for purposes of illustration, and do not illustrate a three body system. The orbital period, a function of the semi-major axis, the aggregate mass of the two body system, and the gravitational constant, is the same for both systems, and independent of eccentricity. Due to Kepler's second law, however, a line joining the orbiting body and the center of mass of the system sweeps out equal areas during equal intervals of time. Consequently, for highly eccentric orbits, an orbiting body near periapsis, and the center of mass necessarily exhibits a large radial velocity. At apoapsis, with the body distant from the center of mass, a correspondingly small angular velocity ensues. This gives rise to a slingshot effect absent in circular orbits of zero eccentricity. The sling-shot effect becomes more marked as eccentricity approaches unity. The plotting system employed R. H. Battin's universal formula to compute position and velocity for equal time steps from the periapsis passage. See Kaplan, Marshall H. Modern Spacecraft Dynamics and Control 1976 John Wiley and Sons ISBN 0-471-45703-5 pp 306 -308. Computations implemented in python, imagery generated using the TK Widget toolkit. Animation composited in Adobe After Effects; animated GIF generated and optimized in Gimp 2.2. |
| Other versions
|
If there are other versions of this media on CZ, please list them here. |
| Using this image on CZ
|
Copy the code below to add this image to a Citizendium article, changing the size, alignment, and caption as necessary.
|
Please send email to manager A T citizendium.org .
Licensing/Copyright status
Comparison of Eccentricity.gif is licenced under the GNU Free Documentation License v2.1 or later
Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, version 2.1 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts.
Read the licence for full details
Notice of CC-by-sa incompatibility
Text on the Citizendium is licensed under the Creative Commons Attribution ShareAlike licence.
This media may not be used under those or closely similar terms without separate permission of the copyright holder, or the user's own fair use determination.
File history
Click on a date/time to view the file as it appeared at that time.
| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 18:51, 11 March 2022 |  | 433 × 289 (36 KB) | Maintenance script (talk | contribs) | == Summary == Importing file |
You cannot overwrite this file.
File usage
The following page uses this file:
