{"id":5384,"date":"2020-04-01T22:00:10","date_gmt":"2020-04-01T22:00:10","guid":{"rendered":"https:\/\/ja.modelondev.com\/blog\/2020\/04\/01\/aircraft-aileron-actuator-real-time-simulation\/"},"modified":"2022-07-13T18:32:02","modified_gmt":"2022-07-13T18:32:02","slug":"aircraft-aileron-actuator-real-time-simulation","status":"publish","type":"post","link":"https:\/\/modelon.com\/ja\/blog\/aircraft-aileron-actuator-real-time-simulation\/","title":{"rendered":"\u822a\u7a7a\u6a5f\u30a8\u30eb\u30ed\u30f3\u30a2\u30af\u30c1\u30e5\u30a8\u30fc\u30bf\u306e\u30ea\u30a2\u30eb\u30bf\u30a4\u30e0\u30b7\u30df\u30e5\u30ec\u30fc\u30b7\u30e7\u30f3"},"content":{"rendered":"<p><em>This blog is Part 4 of a blog series that demonstrates how the <a href=\"https:\/\/modelon.com\/ja\/library\/hydraulics-library\/\">Modelon\u00a0Hydraulics\u00a0Library<\/a> can be used for the model-based development of an Aircraft Hydraulic Actuation System (AHAS). <\/em><em>In this series, basic steps of the actuation system development workflow will be covered.<\/em><\/p>\n<p><em>Previously, <a href=\"https:\/\/modelon.com\/ja\/modeling-and-simulation-of-aircraft-aileron-actuator\/\">Part 2<\/a> and Part 3 focused on the modeling and simulation of electro-hydraulic actuator with datasheet-based parametrization. Part 4 &#8211; below &#8211; is dedicated to simulating the simplified aileron model in a real-time target.<\/em><\/p>\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-actuation-system-architectures-with-modelon-hydraulics-library\/\" >Part 1 - Modeling Actuation System Architectures<\/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\/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<h4>The Importance of Real-Time Simulation<\/h4>\n<p>During the development of a Fly-by-Wire actuator and its control electronics, the trimming of the actuator control laws is of particular importance. While most can be performed with simulation on a standard computer, one relevant step is to include the control laws on a real-time target that controls the physical model (plant model) inputs. These two models are usually not coming from the same software.<\/p>\n<p>This plant model shall react in real-time \u2013 i.e. the computation of every simulated time step takes less time than the simulated time itself \u2013 to avoid that the model would be delayed compared with real-time orders (this would be a task overrun). This real-time integration enables validating the actuator control laws with more accuracy.<\/p>\n<p>In this blog post, we will illustrate how the simple actuator model developed in the blog post 2 is integrated in a Speedgoat target and runs real-time.<\/p>\n<h4>Minor Model Adaptations<\/h4>\n<p>The changes made on the model are the following:<\/p>\n<ul>\n<li>Isolation of the plant model (the simple control logic would be in the real-time target implemented in Simulink\u00ae).<\/li>\n<li>Addition of a few outputs monitoring the pressures, flow rate and force of the plant model \u2013 to have an easier access to and plotting of these.<\/li>\n<\/ul>\n<p>Figure 1 below displays the final version of the model.<\/p>\n<figure id=\"attachment_6618\" aria-describedby=\"caption-attachment-6618\" style=\"width: 464px\" class=\"wp-caption aligncenter\"><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-6618\" src=\"https:\/\/modelon.com\/ja\/wp-content\/uploads\/sites\/3\/2022\/06\/AHAS-Blog-4-Figure-1.png\" alt=\"\" width=\"464\" height=\"375\" \/><figcaption id=\"caption-attachment-6618\" class=\"wp-caption-text\">Figure 1 A320 aileron actuator-like plant model \u2013 ready for export<\/figcaption><\/figure>\n<h4>Integration on the Real-Time Target<\/h4>\n<p>The integration in the Real-Time target consists of a few steps:<\/p>\n<ul>\n<li>Coding in Simulink\u00ae the control\/command blocks of the actuators.<\/li>\n<li>Including the Modelica model made from Modelon Hydraulics, exported as an FMU, using <a href=\"https:\/\/modelon.com\/ja\/products-services\/modelon-deployment-suite\/fmi-toolbox\/\">FMI Toolbox<\/a> developed by Modelon.<\/li>\n<li>Adding Speedgoat specific blocks to monitor the variables of interest.<\/li>\n<li>Build the real time executable using the Simulink Real-Time\u2122 target.<\/li>\n<\/ul>\n<figure id=\"attachment_6620\" aria-describedby=\"caption-attachment-6620\" style=\"width: 624px\" class=\"wp-caption aligncenter\"><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-6620\" src=\"https:\/\/modelon.com\/ja\/wp-content\/uploads\/sites\/3\/2022\/06\/AHAS-Blog-4-Figure-2.png\" alt=\"\" width=\"624\" height=\"374\" \/><figcaption id=\"caption-attachment-6620\" class=\"wp-caption-text\">Figure 2 actuator plant model integration in Simulink for import on Speedgoat real-time target<\/figcaption><\/figure>\n<p>In this application, the plant model has been exported with its own solver (co-simulation) so that both the control and the plant model have separate solvers and the models communicate at each time step.<\/p>\n<h4><span class=\"TextRun SCXW228854465 BCX0\" lang=\"EN-US\" data-contrast=\"none\"><span class=\"NormalTextRun CommentStart SCXW228854465 BCX0\">Real-Time Simulation of the Integrated Systems<br \/>\n<\/span><\/span><\/h4>\n<p>Once the model is integrated and imported on the real-time target, it is run satisfying hard real-time requirements. The main variables set as output previously are plotted here:<\/p>\n<ul>\n<li><span style=\"text-decoration: underline;\">Top left:<\/span> actuator command and response. We observe an initial position of the actuator on-purpose different from the command leading to a fast transient at the beginning of the simulation. After reaching the setpoint, the actuator reacts in a satisfactory dynamic behavior, slightly influenced by the antagonist loads.<\/li>\n<li><span style=\"text-decoration: underline;\">Bottom left<\/span>: the flow exiting the ideal pressure source is plotted. The dynamic observed is a redressed sine similar to the actuator position response. The frequency is doubled as the flow is provided in both positive and negative speeds of the actuator.<\/li>\n<li><span style=\"text-decoration: underline;\">Top right<\/span>: the pressure in both chambers are observed. These are oscillating around an average point, in phase with the force oscillation shown at the <span style=\"text-decoration: underline;\">bottom right.<\/span><\/li>\n<\/ul>\n<div class=\"mceTemp\"><\/div>\n<figure id=\"attachment_6622\" aria-describedby=\"caption-attachment-6622\" style=\"width: 498px\" class=\"wp-caption aligncenter\"><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-6622\" src=\"https:\/\/modelon.com\/ja\/wp-content\/uploads\/sites\/3\/2022\/06\/AHAS-Blog-4-Figure-3.png\" alt=\"\" width=\"498\" height=\"392\" \/><figcaption id=\"caption-attachment-6622\" class=\"wp-caption-text\">Figure 3 plotting of main variables of interests in the Speedgoat GUI<\/figcaption><\/figure>\n<h4><span class=\"TextRun SCXW228854465 BCX0\" lang=\"EN-US\" data-contrast=\"none\"><span class=\"NormalTextRun CommentStart SCXW228854465 BCX0\">Conclusion<br \/>\n<\/span><\/span><\/h4>\n<p>In this short blog post, we have illustrated the capabilities of exporting a Modelon Hydraulics Library model and integrated into Simulink\u00ae for running the control and plant models in co-simulation on a real-time target.<\/p>\n<p>This demonstrator also illustrates that the same model can be used for different use cases \u2013 here, standard simulation and real-time simulation on a HiL target.<\/p>\n<p>Stay tuned to find out the remaining interesting parts of the series covering full system performance analysis and component detailed design.<\/p>\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\u4f5c\u52d5\u30b7\u30b9\u30c6\u30e0\u306e\u30e2\u30c7\u30eb\u30d9\u30fc\u30b9\u306e\u958b\u767a\u306b\u95a2\u3059\u308b\u30d6\u30ed\u30b0\u30b7\u30ea\u30fc\u30baPart 4\u3067\u3059\u3002<\/p>\n","protected":false},"author":50,"featured_media":5389,"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],"class_list":["post-5384","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-blog","tag-aerospace","blog_news_type-aerospace-defense","blog_news_type-hydraulics-library"],"acf":[],"yoast_head":"<!-- This site is optimized with the Yoast SEO Premium plugin v27.2 (Yoast SEO v27.2) - 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