{"id":5239,"date":"2019-05-13T12:57:40","date_gmt":"2019-05-13T12:57:40","guid":{"rendered":"https:\/\/ja.modelondev.com\/blog\/2019\/05\/13\/modeling-actuation-system-architectures-with-modelon-hydraulics-library\/"},"modified":"2022-07-13T18:05:36","modified_gmt":"2022-07-13T18:05:36","slug":"modeling-actuation-system-architectures-with-modelon-hydraulics-library","status":"publish","type":"post","link":"https:\/\/modelon.com\/ja\/blog\/modeling-actuation-system-architectures-with-modelon-hydraulics-library\/","title":{"rendered":"\u6cb9\u5727\u30e9\u30a4\u30d6\u30e9\u30ea\u3092\u7528\u3044\u305f\u30a2\u30af\u30c1\u30e5\u30a8\u30fc\u30b7\u30e7\u30f3\u30b7\u30b9\u30c6\u30e0\u30a2\u30fc\u30ad\u30c6\u30af\u30c1\u30e3\u306e\u30e2\u30c7\u30ea\u30f3\u30b0"},"content":{"rendered":"\n\n<em>This blog is Part 1 of a blog series that will demonstrate how the <a href=\"https:\/\/modelon.com\/library\/hydraulics-library\/\">Modelon Hydraulics Library<\/a> is well suited to the model-based development of an Aircraft Hydraulic Actuation System (AHAS). In this series, <\/em><em> of the actuation system development workflow will be covered. <\/em>\n\n \n\n<em>Part 1, below, will focus on the architectural modeling of AHAS. In the upcoming posts we will cover component detailed design, component integration with datasheet-based parametrization and performance assessment of the entire integrated system.<\/em>\n\n \n    <div class=\"prop-button prop-button__shortcode\">\n\t    \n\t\t<a class=\"button button--solid-primary\" href=\"https:\/\/modelon.com\/ja\/modeling-and-simulation-of-aircraft-aileron-actuator\/\" >Part 2 - Modeling of an Aircraft Aileron Actuator<\/a>\n\n\t\t\t<\/div>\n\n\t\n \n    <div class=\"prop-button prop-button__shortcode\">\n\t    \n\t\t<a class=\"button button--solid-primary\" href=\"https:\/\/modelon.com\/ja\/aircraft-aileron-actuator-mode-valve\/\" >Part 3 - Modeling of an Aircraft Aileron Actuator Mode Valve<\/a>\n\n\t\t\t<\/div>\n\n\t\n \n    <div class=\"prop-button prop-button__shortcode\">\n\t    \n\t\t<a class=\"button button--solid-primary\" href=\"https:\/\/modelon.com\/ja\/aircraft-aileron-actuator-real-time-simulation\/\" >Part 4 - Real-Time Simulation of an Aircraft Aileron Actuator<\/a>\n\n\t\t\t<\/div>\n\n\t\n \n<h4 class=\"wp-block-heading\">Introduction<\/h4>\n \n\nThe actuation system of an aircraft performs a safety critical function that ensures controllability. Although today\u2019s trend is focused on developing electrical actuation systems, \u00a0current aircraft and new developments still require hydraulic power to feed the actuators.\n\n \n<h4 class=\"wp-block-heading\"><em>AHAS<\/em> functional breakdown<\/h4>\n \n\n<a href=\"#_ftn1\" name=\"_ftnref1\"><\/a><span class=\"TextRun SCXW239288324 BCX0\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun CommentStart SCXW239288324 BCX0\">In this series, the\u00a0AHAS is defined as the set of actuators that drives the control surfaces and the associated hydraulic systems. An extensive definition should cover the flight control computer (or similar components that perform the same function) in which the actuator control loops are implemented. For simplification purpose, the actuator control loop will be reduced to block diagrams that will still ensure such a functionality.\u00a0Thus\u00a0AHAS\u00a0covers\u00a0the following main functions:<\/span>\u00a0<\/span>\n\n \n<ul class=\"wp-block-list\">\n \t<li><strong>Store hydraulic fluid<\/strong> \u2013 typically ensured by reservoirs \u2013 pressurized or non-pressurized.<\/li>\n \t<li><strong>Generate hydraulic power<\/strong> \u2013 typically ensured by mechanical pumps, electric pumps, hand pumps, ram air turbine (RAT) and power transfer units (PTU).<\/li>\n \t<li><strong>Store hydraulic power<\/strong> \u2013 mostly covered by accumulators (<span class=\"TextRun SCXW78416834 BCX0\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun SCXW78416834 BCX0\">also by capacitance effect of\u00a0<\/span><\/span><span class=\"TextRun SCXW78416834 BCX0\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun SCXW78416834 BCX0\">the lines<\/span><\/span>).<\/li>\n \t<li><strong>Distribute hydraulic power<\/strong> \u2013 <span class=\"TextRun BCX0 SCXW15854148\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun BCX0 SCXW15854148\">mostly ensured by rigid<\/span><\/span><span class=\"TextRun BCX0 SCXW15854148\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun BCX0 SCXW15854148\">\u00a0lines<\/span><\/span><span class=\"TextRun BCX0 SCXW15854148\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun BCX0 SCXW15854148\">\u00a0and\u00a0<\/span><\/span><span class=\"TextRun BCX0 SCXW15854148\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun BCX0 SCXW15854148\">hoses<\/span><\/span><span class=\"TextRun BCX0 SCXW15854148\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun BCX0 SCXW15854148\">\u00a0as well as dedicated valves to\u00a0<\/span><\/span><span class=\"TextRun BCX0 SCXW15854148\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun CommentStart BCX0 SCXW15854148\">guide\u00a0<\/span><\/span><span class=\"TextRun BCX0 SCXW15854148\" lang=\"EN-US\" data-contrast=\"auto\"><span class=\"NormalTextRun BCX0 SCXW15854148\">the fluid.<\/span><\/span><\/li>\n \t<li><strong>Convert hydraulic power<\/strong> \u2013 typically performed by linear or rotary actuators. It can be split into two sub-functions:\n<ul>\n \t<li><strong>Meter hydraulic power<\/strong> \u2013 typically ensured by proportional control valves.<\/li>\n \t<li><strong>Transform hydraulic power<\/strong> (in to mechanical power) \u2013 usually performed by hydraulic cylinders (linear or rotary).<\/li>\n<\/ul>\n<\/li>\n<\/ul>\n \n<h4 class=\"wp-block-heading\">Architectural modeling of \u00a0AHAS, using Modelon Hydraulics Library<\/h4>\n \n\nWhen developing a system using the Modelica[mfn]All Modelica keywords will be colored in orange in order to highlight them.[\/mfn] language, it is convenient to identify the system topology and build a template for this system. The template introduces placeholders \u2013 usually called base classes \u2013 for the system.\n\n \n\nA best practice is to have a placeholder that includes all common parts for the functions that the subsystems must achieve (e.g. interfaces). Note that this is only possible when subsystem boundaries are drawn such that their functions are independent.\n\n \n\nAll components that are candidates to be template shall extend the base class of the function they fulfill. This enables easy selection of well-suited components by replacing the placeholder by one of the components that extends it, at which point the class will be redeclared accordingly. The same template would then enable building several systems that have the same functional architecture. As a result: 1) models are easily reused between one system to another, 2) model maintenance will be simplified and, 3) the end user can easily configure its system without caring about potential incompatibilities.\n\n \n<figure class=\"wp-block-image alignnone size-full wp-image-5494\"><img decoding=\"async\" class=\"wp-image-5494\" src=\"https:\/\/modelon.com\/wp-content\/uploads\/2022\/06\/AHAS.gif\" alt=\"\" \/>\n<figcaption>Figure 1 \u2013 Functional architecture of the AHAS using Modelon Hydraulics library<\/figcaption><\/figure>\n \n<figure class=\"wp-block-image size-large\"><img decoding=\"async\" class=\"wp-image-10128\" src=\"https:\/\/modelon.com\/wp-content\/uploads\/2022\/07\/Figure-1-1200x644-1-1024x550.png\" alt=\"\" \/><\/figure>\n \n\nThe A320 actuation system includes fifteen control surfaces that are actuated by a total of twenty-one actuators.\u00a0Except for\u00a0the actuators\u00a0that are\u00a0dedicated to the \u201cdirection\u201d control\u00a0surfaces, all other actuators are using electro-hydraulic servo valves (EHSV) in order to meter the hydraulic power coming from the hydraulic system.\n\n \n\nIn order to operate safely, in compliance with the dedicated regulations, the A320 includes three independent, segregated and dissimilar hydraulic systems. Each of those is usually named after a color: the green, blue and yellow circuits. Each circuit feeds different actuators that actuate different control surfaces.\n\n \n\nThis template should be instantiated once per circuit (green, blue and yellow) if the full system should be modeled.\n\n \n<h4 class=\"wp-block-heading\">Multiple connections in one connector<\/h4>\n \n\nWith the proposed architecture, one could wonder how it is possible to model the pressures available at each actuator port of a hydraulic system.\n\n \n\nThis is made possible with the dedicated hierarchical connectors \u2013 which include one connector per actuator (see below), connecting <em>distribute<\/em> and <em>convert<\/em> functional models with a single line. Hierarchal connectors also enable the user to connect to each of the internal connectors within a subsystem, making it possible to reach the correct actuator by selecting the correct name.\n\n \n<figure class=\"wp-block-image\"><img decoding=\"async\" class=\"wp-image-5460\" src=\"https:\/\/modelon.com\/wp-content\/uploads\/2022\/06\/Code-Block-1-1.png\" alt=\"\" \/><\/figure>\n \n<h4 class=\"wp-block-heading\">Conclusion and coming posts<\/h4>\n \n\nPart 1 has demonstrated how to take advantage of some Modelica key features in order to build the functional model of an AHAS.\n\n \n\nIn Part 2, 3, &amp; 4, we will detail the actuator models and then illustrate how this architecture model can be used to study \u00a0AHAS performance in different scenarios.\n\n \n<h4 class=\"wp-block-heading\">Glossary<\/h4>\n \n<figure class=\"wp-block-image size-full\"><img decoding=\"async\" class=\"wp-image-10129\" src=\"https:\/\/modelon.com\/wp-content\/uploads\/2022\/07\/Glossary1.png\" alt=\"\" \/><\/figure>\n","protected":false},"excerpt":{"rendered":"<p>\u3053\u306e\u30d6\u30ed\u30b0\u306f\u3001\u30e2\u30c7\u30ed\u30f3\u306e\u6cb9\u5727\u30e9\u30a4\u30d6\u30e9\u30ea (Hydraulics Library) \u3092\u4f7f\u7528\u3057\u305f\u822a\u7a7a\u6a5f\u306e\u6cb9\u5727\u30a2\u30af\u30c1\u30e5\u30a8\u30fc\u30b7\u30e7\u30f3\u30b7\u30b9\u30c6\u30e0\u306e\u30e2\u30c7\u30eb\u30d9\u30fc\u30b9\u306e\u958b\u767a\u306b\u95a2\u3059\u308b\u30d6\u30ed\u30b0\u30b7\u30ea\u30fc\u30ba Part 1 \u3067\u3059\u3002\u822a\u7a7a\u6a5f\u306e\u5b8c\u5168\u306a\u30a2\u30af\u30c1\u30e5\u30a8\u30fc\u30b7\u30e7\u30f3\u30b7\u30b9\u30c6\u30e0\u3068\u30b5\u30d6\u30b7\u30b9\u30c6\u30e0\u3092\u30e2\u30c7\u30eb\u5316\u3059\u308b\u65b9\u6cd5\u306b\u3064\u3044\u3066\u3054\u7d39\u4ecb\u3057\u307e\u3059\u3002<\/p>\n","protected":false},"author":50,"featured_media":5244,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"_relevanssi_hide_post":"","_relevanssi_hide_content":"","_relevanssi_pin_for_all":"","_relevanssi_pin_keywords":"","_relevanssi_unpin_keywords":"","_relevanssi_related_keywords":"","_relevanssi_related_include_ids":"","_relevanssi_related_exclude_ids":"","_relevanssi_related_no_append":"","_relevanssi_related_not_related":"","_relevanssi_related_posts":"","_relevanssi_noindex_reason":"","inline_featured_image":false,"editor_notices":[],"footnotes":""},"categories":[12],"tags":[42,14],"class_list":["post-5239","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-blog","tag-aerospace","tag-migrate","blog_news_type-aerospace-defense","blog_news_type-aircraft-dynamics-library"],"acf":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO Premium plugin v27.2 (Yoast SEO v27.2) - 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