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Predefined CS-22 requirements, such as a maximum take-off distance of 500 meters, are satisfied by design, while manufacturer or customer requirements can be added. The workflow establishes bidirectional traceability from requirements to test results using Polarion PLM and MATLAB/Simulink mission evaluation with a nonlinear 6-DoF simulation model. Connectivity between tools is provided via SimPol and Tico, and the method is demonstrated with a test run using three requirements.",{"@graph":14,"@context":73},[15,34,56],{"@type":16,"itemListElement":17},"BreadcrumbList",[18,23,27,31],{"item":19,"name":20,"@type":21,"position":22},"https://docshare.wps.com","Home","ListItem",1,{"item":24,"name":25,"@type":21,"position":26},"https://docshare.wps.com/template/","Template",2,{"item":28,"name":29,"@type":21,"position":30},"https://docshare.wps.com/template/presentations/","Presentations",3,{"item":32,"name":10,"@type":21,"position":33},"https://docshare.wps.com/template/certification-compliant-performance-analysis-and-requirements-management-of-an-electrically-powered-general-aviation-aircraft-research-article/240923/",4,{"url":32,"name":10,"@type":35,"image":36,"author":41,"headline":10,"publisher":44,"fileFormat":47,"inLanguage":8,"description":12,"dateModified":48,"datePublished":49,"encodingFormat":47,"isAccessibleForFree":50,"interactionStatistic":51},"DigitalDocument",{"url":37,"@type":38,"width":39,"height":40},"https://docshare.wps.com/thumbnails/certification-compliant-performance-analysis-and-requirements-management-of-an-electrically-powered-general-aviation-aircraft-research-article/240923.png","ImageObject",442,249,{"name":42,"@type":43},"Jacob","Person",{"url":19,"name":45,"@type":46},"DocShare","Organization","application/pdf","2026-10-29","2026-09-11",true,{"@type":52,"interactionType":53,"userInteractionCount":55},"InteractionCounter",{"@type":54},"ViewAction",11,{"@type":57,"mainEntity":58},"FAQPage",[59,65,69],{"name":60,"@type":61,"acceptedAnswer":62},"What is the main purpose of the presented toolchain?","Question",{"text":63,"@type":64},"It validates requirements for certification-compliant performance analysis by providing bidirectional traceability from requirements to test results.","Answer",{"name":66,"@type":61,"acceptedAnswer":67},"Which standards and certification class does the approach target?",{"text":68,"@type":64},"The method targets EASA CS-22 certification for an electric propulsion system used in a general aviation aircraft.",{"name":70,"@type":61,"acceptedAnswer":71},"How is mission performance evaluated in the workflow?",{"text":72,"@type":64},"Mission evaluation is carried out with MATLAB/Simulink using a nonlinear 6-DoF simulation model, linked to requirements management in Polarion PLM.","https://schema.org",{"og:url":32,"og:type":75,"og:title":10,"og:site_name":45,"og:description":12},"article",{"robots":77,"canonical":32},"index,follow",{"doc_id":79,"site_id":7},240923,1791725082,{"code":4,"msg":82,"data":83},"success",[84,87,92,97,102,107,112,117,122],{"id":55,"doc_module":22,"doc_module_name":25,"category_name":29,"show_sort_weight":85,"slug":86},90,"presentations",{"id":88,"doc_module":22,"doc_module_name":25,"category_name":89,"show_sort_weight":90,"slug":91},12,"Resumes",80,"resumes",{"id":93,"doc_module":22,"doc_module_name":25,"category_name":94,"show_sort_weight":95,"slug":96},14,"Invoices",70,"invoices",{"id":98,"doc_module":22,"doc_module_name":25,"category_name":99,"show_sort_weight":100,"slug":101},15,"Posters",60,"posters",{"id":103,"doc_module":22,"doc_module_name":25,"category_name":104,"show_sort_weight":105,"slug":106},16,"Social Media",50,"social-media",{"id":108,"doc_module":22,"doc_module_name":25,"category_name":109,"show_sort_weight":110,"slug":111},17,"Forms",40,"forms",{"id":113,"doc_module":22,"doc_module_name":25,"category_name":114,"show_sort_weight":115,"slug":116},18,"Letters",30,"letters",{"id":118,"doc_module":22,"doc_module_name":25,"category_name":119,"show_sort_weight":120,"slug":121},21,"Paper Templates",5,"papers-templates",{"id":123,"doc_module":22,"doc_module_name":25,"category_name":124,"show_sort_weight":4,"slug":125},158,"General","general-158",{"code":4,"msg":82,"data":127},{"doc_id":79,"user_id":128,"nickname":42,"user_avatar":129,"doc_module":22,"category_id":55,"category_name":29,"doc_title":10,"doc_description":12,"doc_content":130,"file_id":131,"file_url":132,"file_type":133,"file_size":134,"view_count":55,"is_deleted":4,"is_public":22,"is_downloadable":22,"audit_status":22,"page_count":55,"language":135,"language_code":8,"site_id":7,"html_lang":8,"table_of_contents":136,"faqs":137,"seo_title":138,"seo_description":12,"update_tm":139,"read_time":33},962084931830,"https://ap-avatar.wpscdn.com/davatar_a8503ba1806abce46bf441b54a3ca4cd","Journal of Aeronautics and Space Technologies  \n17(Special Issue) (2024) 208-218  \nJournal Homepage: [jast.hho.msu.edu.tr](jast.hho.msu.edu.tr)  \nRESEARCH ARTICLE  \nCertification Compliant Performance Analysis and Requirements Management of an Electrically Powered General Aviation Aircraft  \nElektrikle Çalışan Bir Genel Havacılık Uçağının Sertifikasyona Uygun Performans Analizi ve Gereksinim Yönetimi  \nLuca Hein 1*, Purav Panchal 1 , Prof. Dr. -Ing. Stephan Myschik1  \n1 University of the Bundeswehr Munich, Institute for Aeronautical Engineering  \n85521 Neubiberg, Germany  \nReceived: January 24, 2024 Revised: March 12, 2024 Accepted: March 20, 2024  \nAbstract Öz  \nThis article presents an implementation of a requirements validation toolchain for the certification-compliant performance analysis of an electrically powered general aviation aircraft. As part of the [dtec.bw](dtec.bw) project ELAPSED, a novel approach for an electric propulsion system for an aircraft of the EASA certification specification class CS-22 is developed. Predefined requirements for the aircraft must be met by the design in order to comply with the CS-22 certification rules, such as a maximum take-off distance of 500 meters. Other requirements defined by the manufacturer or customer can also be easily added. A toolchain providing bidirectional traceability from the requirements to the test results has been established to validate the feasibility of the aircraft and system requirements and their compliance with the certification standards. This toolchain consists of Polarion PLM for requirements management and  \nMATLAB/Simulink for mission evaluation using anon-linear 6-DoF simulation model for the respective aircraft. Two in-house tools called SimPol and Tico provide connectivity and roundtripping between Polarion and Simulink. The application of this toolchain is presented in this article using a test run with 3 requirements.  \nKeywords: Requirements, Certification, Polarion, Simulation, Performance Analysis  \nBu makale, elektrikle çalışan bir genel havacılıkuçağının sertifikasyona uygun performans analiziiçin bir gereksinim doğrulama araç zincirininuygulanmasını sunmaktadır. ELAPSED [dtec.bw](dtec.bw)[ ](dtec.bw)projesinin bir parçası olarak, EASA sertifikasyonspesifikasyon sınıfı CS-22 olan bir hava aracı içinelektrikli tahrik sistemine yönelik yeni bir yaklaşım geliştirilmiştir. CS-22 sertifikasyon kurallarına uymak için, maksimum 500 metrelikkalkış mesafesi gibi uçak için önceden tanımlanmış gereklilikler tasarım tarafından karşılanmalıdır. Üretici veya müşteri tarafındantanımlanan diğer gereksinimler de kolaycaeklenebilir. Uçak ve sistem gereksinimlerininuygulanabilirliğini ve sertifikasyon standartlarınauygunluğunu doğrulamak için gereksinimlerden test sonuçlarına çift yönlü izlenebilirlik sağlayan bir araç zinciri oluşturulmuştur. Bu araç zinciri, gereksinim yönetimi için Polarion PLM ve ilgiliuçak için doğrusal olmayan 6-DoF simülasyon modeli kullanarak görev değerlendirmesi için MATLAB/Simulink'ten oluşmaktadır. SimPol ve Tico adlı iki şirket içi araç Polarion ve Simulink arasında bağlantı ve gidiş geliş sağlamaktadır. Bu araç zincirinin uygulaması, bu makalede 3 gereksinimli bir test çalıştırması kullanılaraksunulmuştur.  \nAnahtar Kelimeler: Gereksinimler, Sertifikasyon, Polarion, Simülasyon, Performans Analizi  \n1. INTRODUCTION  \nThe [dtec.bw](dtec.bw) project ELAPSED is concerned with the development of an innovative electric drive chain comprising a multi-stage battery technology and an improved electric motor. This drive train is to be integrated into a powered glider that is currently being developed by an aircraft manufacturer. The electric glider with a take-off mass of 820 kg and a maximum continuous power of 80 kW is aiming for EASA CS-22 certification [1] . To achieve this goal, the development of the aircraft, including the powertrain, must be in accordance with the EASA certification specification and standard. Therefore, several add","cbCaig6jszUF8AU8","https://ap.wps.com/l/cbCaig6jszUF8AU8","pdf",658031,"English","# Certification Compliant Performance Analysis and Requirements Management of an Electrically Powered General Aviation Aircraft\n## Abstract\n## Keywords\n## 1. INTRODUCTION\n## 2. PROJECT STRUCTURE AND WORKFLOW","[{\"question\":\"What is the main purpose of the presented toolchain?\",\"answer\":\"It validates requirements for certification-compliant performance analysis by providing bidirectional traceability from requirements to test results.\"},{\"question\":\"Which standards and certification class does the approach target?\",\"answer\":\"The method targets EASA CS-22 certification for an electric propulsion system used in a general aviation aircraft.\"},{\"question\":\"How is mission performance evaluated in the workflow?\",\"answer\":\"Mission evaluation is carried out with MATLAB/Simulink using a nonlinear 6-DoF simulation model, linked to requirements management in Polarion PLM.\"}]","Certification Compliant Performance Analysis and Requirements Management of an Electrically Powered General Aviation Aircraft - Research Article | PDF",1789167584]