{"id":4420,"date":"2015-04-13T08:51:58","date_gmt":"2015-04-13T12:51:58","guid":{"rendered":"http:\/\/pages.vassar.edu\/magnes\/?p=4420"},"modified":"2015-05-13T23:06:59","modified_gmt":"2015-05-14T03:06:59","slug":"preliminary-results-precession-of-mercurian-planets","status":"publish","type":"post","link":"https:\/\/pages.vassar.edu\/magnes\/2015\/04\/13\/preliminary-results-precession-of-mercurian-planets\/","title":{"rendered":"Preliminary Results: Precession of Mercurian Planets"},"content":{"rendered":"<p>This week I worked on the modeling of Mercury&#8217;s orbital motion around the Sun. Using the Euler-Chromer Method\u00a0and the general relativistic force law (see previous post for a more quantitative description) I was able to create a code that shows Mercury&#8217;s movement over several orbits. The value for alpha was used at 0.01 (very much greater than the true value) and that the initial conditions used were when <img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/pages.vassar.edu\/magnes\/wp-content\/ql-cache\/quicklatex.com-d8aa29214802d40422818752007f00c9_l3.png\" class=\"ql-img-inline-formula \" alt=\"&#32;&#114;&#95;&#123;&#73;&#125;&#61;&#48;&#46;&#52;&#55;&#32;&#65;&#85;&#32;\" title=\"Rendered by QuickLaTeX.com\" height=\"16\" width=\"98\" style=\"vertical-align: -3px;\"\/>,\u00a0and <img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/pages.vassar.edu\/magnes\/wp-content\/ql-cache\/quicklatex.com-49624598409d3baeefd9c4fd0ba07a92_l3.png\" class=\"ql-img-inline-formula \" alt=\"&#32;&#86;&#95;&#123;&#73;&#125;&#61;&#56;&#46;&#50;&#32;\" title=\"Rendered by QuickLaTeX.com\" height=\"15\" width=\"64\" style=\"vertical-align: -3px;\"\/> <img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/pages.vassar.edu\/magnes\/wp-content\/ql-cache\/quicklatex.com-bf3b74a83eda34ca842907cd181bf64c_l3.png\" class=\"ql-img-inline-formula \" alt=\"&#32;&#92;&#102;&#114;&#97;&#99;&#123;&#65;&#85;&#125;&#123;&#121;&#101;&#97;&#114;&#125;&#32;\" title=\"Rendered by QuickLaTeX.com\" height=\"25\" width=\"28\" style=\"vertical-align: -9px;\"\/>. It is clear over several orbits that the location of Mercury&#8217;s perihelion is changing.<\/p>\n<p>In the following plot, the different positions for the\u00a0aphelion (chosen for clarity)\u00a0are clearly\u00a0shown by lines connecting the origin (or the Sun) to the aphelion.<\/p>\n<p><a href=\"http:\/\/pages.vassar.edu\/magnes\/files\/2015\/04\/MercuryPeri3.jpg\"><img loading=\"lazy\" decoding=\"async\" class=\"alignnone size-medium wp-image-4495\" src=\"http:\/\/pages.vassar.edu\/magnes\/files\/2015\/04\/MercuryPeri3-300x169.jpg\" alt=\"MercuryPeri3\" width=\"300\" height=\"169\" srcset=\"https:\/\/pages.vassar.edu\/magnes\/files\/2015\/04\/MercuryPeri3-300x169.jpg 300w, https:\/\/pages.vassar.edu\/magnes\/files\/2015\/04\/MercuryPeri3-1024x576.jpg 1024w, https:\/\/pages.vassar.edu\/magnes\/files\/2015\/04\/MercuryPeri3-624x351.jpg 624w, https:\/\/pages.vassar.edu\/magnes\/files\/2015\/04\/MercuryPeri3.jpg 1366w\" sizes=\"auto, (max-width: 300px) 100vw, 300px\" \/><\/a><\/p>\n<p>It is my next goal to determine the amount of degrees by which\u00a0the orientation of this orbit changes over time. I have run into the issue\u00a0that Matlab&#8217;s acos and asin (arccos and arcsin) functions\u00a0give imaginary values if their inputs are\u00a0not with the range of -1&lt;x&lt;1. When this issue is resolved, I will be able to\u00a0finish deriving the precession rate of Mercury, and will proceed to experimenting with\u00a0the eccentricity of Mercurian planet orbits and their resulting\u00a0rates of precession.<\/p>\n<p>Here is a link to my Matlab code: https:\/\/docs.google.com\/a\/vassar.edu\/document\/d\/1fw8L5ZvhqMMVMYltkJH6Ac425KrmnbbDUJs_6GV7aPI\/edit?usp=sharing<\/p>\n","protected":false},"excerpt":{"rendered":"<p>This week I worked on the modeling of Mercury&#8217;s orbital motion around the Sun. Using the Euler-Chromer Method\u00a0and the general relativistic force law (see previous post for a more quantitative description) I was able to create a code that shows Mercury&#8217;s movement over several orbits. The value for alpha was used at 0.01 (very much [&hellip;]<\/p>\n","protected":false},"author":2308,"featured_media":0,"comment_status":"open","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[1],"tags":[],"class_list":["post-4420","post","type-post","status-publish","format-standard","hentry","category-uncategorized"],"_links":{"self":[{"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/posts\/4420","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/users\/2308"}],"replies":[{"embeddable":true,"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/comments?post=4420"}],"version-history":[{"count":9,"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/posts\/4420\/revisions"}],"predecessor-version":[{"id":5053,"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/posts\/4420\/revisions\/5053"}],"wp:attachment":[{"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/media?parent=4420"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/categories?post=4420"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/pages.vassar.edu\/magnes\/wp-json\/wp\/v2\/tags?post=4420"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}