An Overview of Calculation Analyses and Tests of the Sw-4 Solo Helicopter in Various Configurations

preprint OA: closed CC-BY-4.0
📄 Open PDF Full text JSON View at publisher

Abstract

Abstract This article presents an overview of issues related to the trials of the SW-4 SOLO helicopter in various configurations resulting from HELIMARIS and Remotely Piloted Aircraft System (RPAS) In Air projects. It covers a wide range of activities carried out by Engineering and Flight Line teams, both in the areas of calculation analyses and as a result of simulation studies, flight and ground tests. The document covers findings of two projects, in which the SW-4 SOLO helicopter took part. One of them is the OCEAN2020 Project, in particular the part concerning the HELIMARIS stage with helicopter modification for the needs of over water operational capabilities. The other is the RPAS In Air Project, where the main configuration changes were the innovative implementation of the system for satellite communication, and a series of tests demonstrating the possibility of controlling an unmanned aerial vehicle with the use of a satellite data link. Over water operations include cooperation with vessels, which was facilitated in the present research project using the T-23 class corvette. Numerical analyses presented in the paper, followed by simulator and flight test campaigns, ensured that the performance objectives of the system were met, as well as compliance with the safety objectives required by authorities. In particular, flight mechanics of the platform were positively evaluated in terms of control margins, stability, and time response in the case of Emergency Floatation System (EFS) malfunction. Different Automatic Flight Control System (AFCS) settings and pilot delay times were examined, and conclusions for further system developments were stated.
Full text 11,927 characters · extracted from preprint-html · click to expand
An Overview of Calculation Analyses and Tests of the Sw-4 Solo Helicopter in Various Configurations | Research Square window.SnipcartSettings = { analytics: { enabled: false } }; (function() { var accessVector = localStorage.getItem('access_vector') || ''; window.dataLayer = window.dataLayer || []; if (accessVector) { window.dataLayer.push({ user: { profile: { profileInfo: { snid: accessVector } } } }); } })(); (function(w,d,s,l,i){w[l]=w[l]||[];w[l].push({'gtm.start':new Date().getTime(),event:'gtm.js'});var f=d.getElementsByTagName(s)[0],j=d.createElement(s),dl=l!='dataLayer'?'&l='+l:'';j.async=true;j.src='https://www.googletagmanager.com/gtm.js?id='+i+dl;f.parentNode.insertBefore(j,f);})(window,document,'script','dataLayer','GTM-K279D39R'); Browse Preprints In Review Journals COVID-19 Preprints AJE Video Bytes Research Tools Research Promotion AJE Professional Editing AJE Rubriq About Preprint Platform In Review Editorial Policies Our Team Advisory Board Help Center Sign In Submit a Preprint Cite Share Download PDF Research Article An Overview of Calculation Analyses and Tests of the Sw-4 Solo Helicopter in Various Configurations ADAM ROSŁOWICZ, RADOSŁAW RACZYŃSKI, WIESŁAW KANADYS, JAKUB SOLARSKI This is a preprint; it has not been peer reviewed by a journal. https://doi.org/ 10.21203/rs.3.rs-6460097/v1 This work is licensed under a CC BY 4.0 License Status: Published Journal Publication published 08 Sep, 2025 Read the published version in CEAS Aeronautical Journal → Version 1 posted You are reading this latest preprint version Abstract This article presents an overview of issues related to the trials of the SW-4 SOLO helicopter in various configurations resulting from HELIMARIS and Remotely Piloted Aircraft System (RPAS) In Air projects. It covers a wide range of activities carried out by Engineering and Flight Line teams, both in the areas of calculation analyses and as a result of simulation studies, flight and ground tests. The document covers findings of two projects, in which the SW-4 SOLO helicopter took part. One of them is the OCEAN2020 Project, in particular the part concerning the HELIMARIS stage with helicopter modification for the needs of over water operational capabilities. The other is the RPAS In Air Project, where the main configuration changes were the innovative implementation of the system for satellite communication, and a series of tests demonstrating the possibility of controlling an unmanned aerial vehicle with the use of a satellite data link. Over water operations include cooperation with vessels, which was facilitated in the present research project using the T-23 class corvette. Numerical analyses presented in the paper, followed by simulator and flight test campaigns, ensured that the performance objectives of the system were met, as well as compliance with the safety objectives required by authorities. In particular, flight mechanics of the platform were positively evaluated in terms of control margins, stability, and time response in the case of Emergency Floatation System (EFS) malfunction. Different Automatic Flight Control System (AFCS) settings and pilot delay times were examined, and conclusions for further system developments were stated. Unmanned Rotorcraft CFD Flight Mechanics Satellite Communication Full Text Additional Declarations No competing interests reported. Cite Share Download PDF Status: Published Journal Publication published 08 Sep, 2025 Read the published version in CEAS Aeronautical Journal → Version 1 posted You are reading this latest preprint version Research Square lets you share your work early, gain feedback from the community, and start making changes to your manuscript prior to peer review in a journal. As a division of Research Square Company, we’re committed to making research communication faster, fairer, and more useful. We do this by developing innovative software and high quality services for the global research community. Our growing team is made up of researchers and industry professionals working together to solve the most critical problems facing scientific publishing. Also discoverable on Platform About Our Team In Review Editorial Policies Advisory Board Help Center Resources Author Services Accessibility API Access RSS feed Manage Cookie Preferences © Research Square 2026 | ISSN 2693-5015 (online) Privacy Policy Terms of Service Do Not Sell My Personal Information {"props":{"pageProps":{"initialData":{"identity":"rs-6460097","acceptedTermsAndConditions":true,"allowDirectSubmit":true,"archivedVersions":[],"articleType":"Research Article","associatedPublications":[],"authors":[{"id":447539587,"identity":"6b1ca6e4-ffc3-4d27-8c1b-5cb87b557b24","order_by":0,"name":"ADAM ROSŁOWICZ","email":"","orcid":"","institution":"","correspondingAuthor":false,"prefix":"","firstName":"ADAM","middleName":"","lastName":"ROSŁOWICZ","suffix":""},{"id":447539589,"identity":"23d85ed7-e754-4606-8811-dd7f63d7b6f4","order_by":1,"name":"RADOSŁAW RACZYŃSKI","email":"","orcid":"","institution":"","correspondingAuthor":false,"prefix":"","firstName":"RADOSŁAW","middleName":"","lastName":"RACZYŃSKI","suffix":""},{"id":447539592,"identity":"f17e59a7-fce7-4436-9a86-80af1aefe1c7","order_by":2,"name":"WIESŁAW KANADYS","email":"","orcid":"","institution":"","correspondingAuthor":false,"prefix":"","firstName":"WIESŁAW","middleName":"","lastName":"KANADYS","suffix":""},{"id":447539594,"identity":"405f7857-c54a-48bf-8a25-43223f309134","order_by":3,"name":"JAKUB SOLARSKI","email":"data:image/png;base64,iVBORw0KGgoAAAANSUhEUgAAAZAAAAAyAQMAAABI0h/eAAAABlBMVEX///8AAABVwtN+AAAACXBIWXMAAA7EAAAOxAGVKw4bAAABE0lEQVRIiWNgGAWjYBACxgY2BmYQgw/MMbCRgYizEaGFDaIljYegFpAkkhaGw4S1MLcfS5MuYKiTY2M/+/jjjILzPPzsvQc/V5TZMPC3dydgdVhP2jHpGQyHjdl40s0kNxjc5pHsOZcseeZcGoPEmbMbsPslvU2ah+FAYhtDGhvjA6AWgxs5BpKNbYcZDCRysWvpfw7SUpfYxv+M+eMDg3M89jdyjH/i1TID6DAeBubENok0BqDDDvAYSOSY4bdlxrNk6xkGQL9IPGOTnGGQzCNx5oyZZcO5NB5cfjHsTzO8XVBRJ8fPn8b8seePnRx/e4/xzYYyGyCjF7uWBhBpgEWGB5tyEJDHJTEKRsEoGAWjAA4AU79YbMe+jZ4AAAAASUVORK5CYII=","orcid":"","institution":"","correspondingAuthor":true,"prefix":"","firstName":"JAKUB","middleName":"","lastName":"SOLARSKI","suffix":""}],"badges":[],"createdAt":"2025-04-16 06:23:26","currentVersionCode":1,"declarations":"","doi":"10.21203/rs.3.rs-6460097/v1","doiUrl":"https://doi.org/10.21203/rs.3.rs-6460097/v1","draftVersion":[],"editorialEvents":[{"content":"https://doi.org/10.1007/s13272-025-00885-4","type":"published","date":"2025-09-08T15:57:06+00:00"}],"editorialNote":"","failedWorkflow":false,"files":[{"id":91358979,"identity":"8cc5f3f0-66ff-47a0-8999-2bf7cc6f4d34","added_by":"auto","created_at":"2025-09-15 16:02:50","extension":"pdf","order_by":1,"title":"","display":"","copyAsset":false,"role":"manuscript-pdf","size":2050081,"visible":true,"origin":"","legend":"","description":"","filename":"CEASSOLOfullpaper.pdf","url":"https://assets-eu.researchsquare.com/files/rs-6460097/v1_covered_126e6164-2a89-4d93-89d7-6dd97bcd76d3.pdf"}],"financialInterests":"No competing interests reported.","formattedTitle":"\u003cp\u003eAn Overview of Calculation Analyses and Tests of the Sw-4 Solo Helicopter in Various Configurations\u003c/p\u003e","fulltext":[],"fulltextSource":"","fullText":"","funders":[],"hasAdminPriorityOnWorkflow":false,"hasManuscriptDocX":false,"hasOptedInToPreprint":true,"hasPassedJournalQc":"","hasAnyPriority":false,"hideJournal":true,"highlight":"","institution":"","isAcceptedByJournal":true,"isAuthorSuppliedPdf":true,"isDeskRejected":"","isHiddenFromSearch":false,"isInQc":false,"isInWorkflow":false,"isPdf":true,"isPdfUpToDate":true,"isWithdrawnOrRetracted":false,"journal":{"display":true,"email":"[email protected]","identity":"researchsquare","isNatureJournal":false,"hasQc":true,"allowDirectSubmit":true,"externalIdentity":"","sideBox":"","snPcode":"","submissionUrl":"/submission","title":"Research Square","twitterHandle":"researchsquare","acdcEnabled":true,"dfaEnabled":false,"editorialSystem":"","reportingPortfolio":"","inReviewEnabled":false,"inReviewRevisionsEnabled":true},"keywords":"Unmanned Rotorcraft, CFD, Flight Mechanics, Satellite Communication","lastPublishedDoi":"10.21203/rs.3.rs-6460097/v1","lastPublishedDoiUrl":"https://doi.org/10.21203/rs.3.rs-6460097/v1","license":{"name":"CC BY 4.0","url":"https://creativecommons.org/licenses/by/4.0/"},"manuscriptAbstract":"\u003cp\u003eThis article presents an overview of issues related to the trials of the SW-4 SOLO helicopter in various configurations resulting from HELIMARIS and Remotely Piloted Aircraft System (RPAS) In Air projects. It covers a wide range of activities carried out by Engineering and Flight Line teams, both in the areas of calculation analyses and as a result of simulation studies, flight and ground tests. The document covers findings of two projects, in which the SW-4 SOLO helicopter took part. One of them is the OCEAN2020 Project, in particular the part concerning the HELIMARIS stage with helicopter modification for the needs of over water operational capabilities. The other is the RPAS In Air Project, where the main configuration changes were the innovative implementation of the system for satellite communication, and a series of tests demonstrating the possibility of controlling an unmanned aerial vehicle with the use of a satellite data link. Over water operations include cooperation with vessels, which was facilitated in the present research project using the T-23 class corvette. Numerical analyses presented in the paper, followed by simulator and flight test campaigns, ensured that the performance objectives of the system were met, as well as compliance with the safety objectives required by authorities. In particular, flight mechanics of the platform were positively evaluated in terms of control margins, stability, and time response in the case of Emergency Floatation System (EFS) malfunction. Different Automatic Flight Control System (AFCS) settings and pilot delay times were examined, and conclusions for further system developments were stated.\u003c/p\u003e","manuscriptTitle":"An Overview of Calculation Analyses and Tests of the Sw-4 Solo Helicopter in Various Configurations","msid":"","msnumber":"","nonDraftVersions":[{"code":1,"date":"2025-04-28 12:59:55","doi":"10.21203/rs.3.rs-6460097/v1","editorialEvents":[{"type":"communityComments","content":0}],"status":"published","journal":{"display":true,"email":"[email protected]","identity":"researchsquare","isNatureJournal":false,"hasQc":true,"allowDirectSubmit":true,"externalIdentity":"","sideBox":"","snPcode":"","submissionUrl":"/submission","title":"Research Square","twitterHandle":"researchsquare","acdcEnabled":true,"dfaEnabled":false,"editorialSystem":"","reportingPortfolio":"","inReviewEnabled":false,"inReviewRevisionsEnabled":true}}],"origin":"","ownerIdentity":"fdfe3e6e-3d1d-4b54-b19a-812d9838e72b","owner":[],"postedDate":"April 28th, 2025","published":true,"recentEditorialEvents":[],"rejectedJournal":[],"revision":"","amendment":"","status":"posted","subjectAreas":[],"tags":[],"updatedAt":"2025-09-15T15:58:45+00:00","versionOfRecord":{"articleIdentity":"rs-6460097","link":"https://doi.org/10.1007/s13272-025-00885-4","journal":{"identity":"ceas-aeronautical-journal","isVorOnly":false,"title":"CEAS Aeronautical Journal"},"publishedOn":"2025-09-08 15:57:06","publishedOnDateReadable":"September 8th, 2025"},"versionCreatedAt":"2025-04-28 12:59:55","video":"","vorDoi":"10.1007/s13272-025-00885-4","vorDoiUrl":"https://doi.org/10.1007/s13272-025-00885-4","workflowStages":[]},"version":"v1","identity":"rs-6460097","journalConfig":"researchsquare"},"__N_SSP":true},"page":"/article/[identity]/[[...version]]","query":{"redirect":"/article/rs-6460097","identity":"rs-6460097","version":["v1"]},"buildId":"8U1c8b4HqxoKbykW_rLl7","isFallback":false,"isExperimentalCompile":false,"dynamicIds":[84888],"gssp":true,"scriptLoader":[]}

Text is read by the "Ask this paper" AI Q&A widget below. Extraction quality varies by source — PMC NXML preserves structure cleanly, OA-HTML may include some navigation residue, and OA-PDF can have broken hyphenation. The publisher copy (via DOI) is the canonical version.

My notes (saved in your browser only)

Ask this paper AI returns verbatim quotes from the full text · source: preprint-html

Answers must be backed by verbatim quotes from this paper's full text. Hallucinated quotes are dropped automatically; if no verbatim passage answers the question, we say so. How this works

Citation neighborhood (no data yet)

We don't have any in-corpus citations linked to this paper yet. This is a recent paper (2025) — citers typically take a year or two to land, and the OpenAlex reference graph may still be filling in.

Source provenance

europepmc
last seen: 2026-05-20T01:45:00.602351+00:00
unpaywall
last seen: 2026-05-27T02:00:06.600101+00:00
License: CC-BY-4.0