{"version":"1.0","provider_name":"CeREF Technique","provider_url":"https:\/\/ceref.helha.be\/technique","author_name":"Maxim DUMORTIER","author_url":"https:\/\/ceref.helha.be\/technique\/author\/dumortierm\/","title":"Conception et optimisation d\u2019architectures multi-onduleurs multi-moteurs pour applications satellites - CeREF Technique","type":"rich","width":600,"height":338,"html":"<blockquote class=\"wp-embedded-content\" data-secret=\"H87qlnmvGv\"><a href=\"https:\/\/ceref.helha.be\/technique\/projets\/fhe-sathimm\/\">Conception et optimisation d\u2019architectures multi-onduleurs multi-moteurs pour applications satellites<\/a><\/blockquote><iframe sandbox=\"allow-scripts\" security=\"restricted\" src=\"https:\/\/ceref.helha.be\/technique\/projets\/fhe-sathimm\/embed\/#?secret=H87qlnmvGv\" width=\"600\" height=\"338\" title=\"\u00ab\u00a0Conception et optimisation d\u2019architectures multi-onduleurs multi-moteurs pour applications satellites\u00a0\u00bb &#8212; CeREF Technique\" data-secret=\"H87qlnmvGv\" frameborder=\"0\" marginwidth=\"0\" marginheight=\"0\" scrolling=\"no\" class=\"wp-embedded-content\"><\/iframe><script type=\"text\/javascript\">\n\/* <![CDATA[ *\/\n\/*! This file is auto-generated *\/\n!function(d,l){\"use strict\";l.querySelector&&d.addEventListener&&\"undefined\"!=typeof URL&&(d.wp=d.wp||{},d.wp.receiveEmbedMessage||(d.wp.receiveEmbedMessage=function(e){var t=e.data;if((t||t.secret||t.message||t.value)&&!\/[^a-zA-Z0-9]\/.test(t.secret)){for(var s,r,n,a=l.querySelectorAll('iframe[data-secret=\"'+t.secret+'\"]'),o=l.querySelectorAll('blockquote[data-secret=\"'+t.secret+'\"]'),c=new RegExp(\"^https?:$\",\"i\"),i=0;i<o.length;i++)o[i].style.display=\"none\";for(i=0;i<a.length;i++)s=a[i],e.source===s.contentWindow&&(s.removeAttribute(\"style\"),\"height\"===t.message?(1e3<(r=parseInt(t.value,10))?r=1e3:~~r<200&&(r=200),s.height=r):\"link\"===t.message&&(r=new URL(s.getAttribute(\"src\")),n=new URL(t.value),c.test(n.protocol))&&n.host===r.host&&l.activeElement===s&&(d.top.location.href=t.value))}},d.addEventListener(\"message\",d.wp.receiveEmbedMessage,!1),l.addEventListener(\"DOMContentLoaded\",function(){for(var e,t,s=l.querySelectorAll(\"iframe.wp-embedded-content\"),r=0;r<s.length;r++)(t=(e=s[r]).getAttribute(\"data-secret\"))||(t=Math.random().toString(36).substring(2,12),e.src+=\"#?secret=\"+t,e.setAttribute(\"data-secret\",t)),e.contentWindow.postMessage({message:\"ready\",secret:t},\"*\")},!1)))}(window,document);\n\/* ]]> *\/\n<\/script>\n","description":"A bord des satellites, les syst\u00e8mes d\u2019orientation des panneaux photovolta\u00efques et des antennes font un grand usage des moteurs pas-\u00e0-pas. Ceux-ci pr\u00e9sentent en effet les performances requises par ce type d\u2019application. Actuellement, la fiabilit\u00e9 de ces syst\u00e8mes est assur\u00e9e par une redondance classique, en d\u00e9doublant les enroulements moteurs et les onduleurs de puissance. Une moiti\u00e9 [&hellip;]","thumbnail_url":"https:\/\/ceref.helha.be\/technique\/app\/uploads\/2021\/03\/SATHIMM-Satelite.jpg"}