{"version":"1.0","provider_name":"\u898f\u683c\u30de\u30b9\u30bf\u30fc","provider_url":"https:\/\/kikakumaster.com\/ja\/","author_name":"KikakuAdmin000","author_url":"https:\/\/kikakumaster.com\/ja\/author\/kikakuadmin000\/","title":"STANAG-4218 - ACCELEROMETER TEST PROCEDURE FOR AN AIRCRAFT INERTIAL NAVIGATION SYSTEM (NO S\/S DOCUMENT) - \u898f\u683c\u30de\u30b9\u30bf\u30fc","type":"rich","width":600,"height":338,"html":"<blockquote class=\"wp-embedded-content\" data-secret=\"WHCL2N4DWl\"><a href=\"https:\/\/kikakumaster.com\/ja\/mil-spec\/stanag-4218\/\">STANAG-4218 &#8211; ACCELEROMETER TEST PROCEDURE FOR AN AIRCRAFT INERTIAL NAVIGATION SYSTEM (NO S\/S DOCUMENT)<\/a><\/blockquote><iframe sandbox=\"allow-scripts\" security=\"restricted\" src=\"https:\/\/kikakumaster.com\/ja\/mil-spec\/stanag-4218\/embed\/#?secret=WHCL2N4DWl\" width=\"600\" height=\"338\" title=\"&#8220;STANAG-4218 &#8211; ACCELEROMETER TEST PROCEDURE FOR AN AIRCRAFT INERTIAL NAVIGATION SYSTEM (NO S\/S DOCUMENT)&#8221; &#8212; \u898f\u683c\u30de\u30b9\u30bf\u30fc\" data-secret=\"WHCL2N4DWl\" 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\/\/# sourceURL=https:\/\/kikakumaster.com\/wp-includes\/js\/wp-embed.min.js\n\/* ]]> *\/\n<\/script>\n","description":"ACCELEROMETER TEST PROCEDURE FOR AN AIRCRAFT INERTIAL NAVIGATION SYSTEM (NO S\/S DOCUMENT) - The aim of this agreement is to define the functional specification (including performance) for Accelerometer Test Procedures to be used in support of an inertial navigation system applicable to aircraft including heleicopters."}