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The Tricopter: an Agile UAV 117 6.1 Design of the Tricopter
ECOLE DOCTORALE UNIVERSITÉ PARIS-SUD ÉCOLE DOCTORALE : Sciences et Technologie de l’Information, des Télécommunications et des Systèmes Laboratoire des Signaux et Systèmes (L2S) Centre de Robotique MinesParisTech (CAOR) DISCIPLINE : Physique THÈSE DE DOCTORAT Présentée et soutenue publiquement par Étienne SERVAIS le 18 septembre 2015. TRAJECTORY PLANNING AND CONTROL OF COLLABORATIVE SYSTEMS: APPLICATION TO TRIROTOR UAVS. Directeurs de thèse : Brigitte d’ANDRÉA-NOVEL Professeur (Mines ParisTech) Hugues MOUNIER Professeur (Université Paris XI) Composition du jury : Rapporteurs : Tarek HAMEL Professeur (Université de Nice Sophia Antipolis) Miroslav KRSTIC´ Professeur (Université de Californie à San Diego) Examinateurs : Jean-Michel CORON Professeur (Université Pierre et Marie Curie) Joachim RUDOLPH Professeur (Université de la Sarre) Claude SAMSON Directeur de recherche (INRIA) Membres invités : Silviu-Iulian NICULESCU Directeur de recherche (CNRS) Arnaud QUADRAT Ingénieur (Sagem-DS) Planification de trajectoire et contrôle d’un système collaboratif : Application à un drone trirotor. Résumé : L’objet de cette thèse est de proposer un cadre complet, du haut niveau au bas niveau, de génération de trajectoires pour un groupe de systèmes dynamiques indé- pendants. Ce cadre, basé sur la résolution de l’équation de Burgers pour la génération de trajectoires, est appliqué à un modèle original de drone trirotor et utilise la platitude des deux systèmes différentiels considérés. La première partie du manuscrit est consacrée à la génération de trajectoires. Celle-ci est effectuée en créant formellement, par le biais de la platitude du système considéré, des so- lutions à l’équation de la chaleur. Ces solutions sont transformées en solution de l’équation de Burgers par la transformation de Hopf-Cole pour correspondre aux formations voulues. -
AEROSPACE July Cover.Indd
www.aerosociety.com ‘X’ MARKS THE SPOT ONBOARD THE A350 AS IT ENTERS FINAL TESTING August 2014 CIVIL UAVs AND THE LAW SYRIA’S AIR FORCE HONEYWELL AT 100 YEARS THE NATIONAL AEROSPACE LIBRARY FARNBOROUGH FULL LIBRARY CATALOGUE NOW AVAILABLE ONLINE. VISIT WWW.AEROSOCIETY.COM/NAL TO BROWSE THE COLLECTION The National Aerospace Library houses an extensive collection devoted to aeronautics, aviation and aerospace technology. This includes: › Over 20,000 aeronautical books › A vast collection of key aviation journals › Over 40,000 technical reports › Extensive holdings of Air Publications, ATA handling notes and air accident reports › Extensive current holdings of International Civil Aviation Organization (ICAO) Documents / Annexes / Circulars › Notices to Airmen / The Air Pilot / UK Aeronautical Information Publication (AIP) › A complete set of Jane’s All The World’s Aircraft › Historically important past minutes of the Society of British Aircraft Constructors / Aerospace Companies (SBAC) Council and its various committees dating from 1916-2000 › Located at Farnborough Business Park, in the former Royal Aircraft Establishment Building now known as ‘The Hub’ www.aerosociety.com/nal The National Aerospace Library The Hub, Fowler Avenue, T +44 (0)1252 701038 Opening hours Farnborough Business Park, E [email protected] Tuesday - Friday 10:00 - 16:00 Farnborough, Hants GU14 7JP www.aerosociety.com/nal United Kingdom Volume 41 Number 8 August 2014 Boeing Green dreams Honeywell Honeywell at 100 Boeing tests of Future technology new environmental under development at performance technology 20 Honeywell. 28 on a series of different aircraft platforms. Contents Correspondence on all aerospace matters is welcome at: The Editor, AEROSPACE, No.4 Hamilton Place, London W1J 7BQ, UK [email protected] Comment Regulars 4 Radome 12 Transmission The latest aviation and Your letters, emails, tweets aeronautical intelligence, and feedback. -
Recent Developments in Aerial Robotics: a Survey and Prototypes Overview Chun Fui Liew, Danielle Delatte, Naoya Takeishi, Takehisa Yairi
1 Recent Developments in Aerial Robotics: A Survey and Prototypes Overview Chun Fui Liew, Danielle DeLatte, Naoya Takeishi, Takehisa Yairi Abstract—In recent years, research and development in aerial cite all related papers in a short paper. To date, there is no sur- robotics (i.e., unmanned aerial vehicles, UAVs) has been growing vey that attempt to list all the UAV papers in a systematic way. at an unprecedented speed, and there is a need to summarize In this work, we systematically identify 1,318 UAV papers that the background, latest developments, and trends of UAV research. Along with a general overview on the definition, types, categories, appear in the top robotic journals/conferences since 2001. The and topics of UAV, this work describes a systematic way to identification process includes screening paper abstracts with identify 1,318 high-quality UAV papers from more than thirty a program script and eliminating non-UAV papers based on thousand that have been appeared in the top journals and several criteria with meticulous human checks. We categorize conferences. On top of that, we provide a bird’s-eye view of the selected UAV papers in several ways, e.g., with regard UAV research since 2001 by summarizing various statistical information, such as the year, type, and topic distribution of to UAV types, research topics, onboard camera systems, off- the UAV papers. We make our survey list public and believe that board motion capture system, countries, years, etc. In addition, the list can not only help researchers identify, study, and compare we provide a high-level view of UAV research since 2001 by their work, but is also useful for understanding research trends summarizing various statistical information, including year, in the field. -
A Review of the Magnus Effect in Aeronautics
Progress in Aerospace Sciences 55 (2012) 17–45 Contents lists available at SciVerse ScienceDirect Progress in Aerospace Sciences journal homepage: www.elsevier.com/locate/paerosci A review of the Magnus effect in aeronautics Jost Seifert n EADS Cassidian Air Systems, Technology and Innovation Management, MEI, Rechliner Str., 85077 Manching, Germany article info abstract Available online 14 September 2012 The Magnus effect is well-known for its influence on the flight path of a spinning ball. Besides ball Keywords: games, the method of producing a lift force by spinning a body of revolution in cross-flow was not used Magnus effect in any kind of commercial application until the year 1924, when Anton Flettner invented and built the Rotating cylinder first rotor ship Buckau. This sailboat extracted its propulsive force from the airflow around two large Flettner-rotor rotating cylinders. It attracted attention wherever it was presented to the public and inspired scientists Rotor airplane and engineers to use a rotating cylinder as a lifting device for aircraft. This article reviews the Boundary layer control application of Magnus effect devices and concepts in aeronautics that have been investigated by various researchers and concludes with discussions on future challenges in their application. & 2012 Elsevier Ltd. All rights reserved. Contents 1. Introduction .......................................................................................................18 1.1. History .....................................................................................................18 -
Guide to The
Guide to the St. Martin WWI Photographic Negative Collection 1914-1918 7.2 linear feet Accession Number: 66-98 Collection Number: FW66-98 Arranged by Jack McCracken, Ken Rice, and Cam McGill Described by Paul A. Oelkrug July 2004 Citation: The St. Martin WWI Photographic Negative Collection, FW66-98, Box number, Photograph number, History of Aviation Collection, Special Collections Department, McDermott Library, The University of Texas at Dallas. Special Collections Department McDermott Library, The University of Texas at Dallas Revised 8/20/04 Table of Contents Additional Sources ...................................................................................................... 3 Series Description ....................................................................................................... 3 Scope and Content ...................................................................................................... 4 Provenance Statement ................................................................................................. 4 Literary Rights Statement ........................................................................................... 4 Note to the Researcher ................................................................................................ 4 Container list ............................................................................................................... 5 2 Additional Sources Ed Ferko World War I Collection, George Williams WWI Aviation Archives, The History of Aviation Collection, -
Charting the Future of Flight
12–14 AUGUST 2O13 LOS ANGELES, CALIFORNIA CHARTING THE FUTURE OF FLIGHT FINAL PROGRAM Sponsored by www.aiaa.org/aviation2013 #aiaaAviation GET YOUR CONFERENCE INFO ON THE GO! Download the FREE AIAA 2013 Conference Mobile App FEATURES • Browse Program – View the program at your fingertips • My Itinerary – Create your own conference schedule • Conference Info – Including special events • Take Notes – Take notes during sessions • Venue Map – Hyatt Regency Century Plaza • City Map – See the surrounding area • Connect to Twitter – Tweet about what you’re doing and who you’re meeting with #aiaaAviation HOW TO DOWNLOAD Any version can be run without an active Internet connection! You can also sync an itinerary you created online with the app by entering your unique itinerary name. Compatible with MyItinerary Mobile App MyItinerary Web App • For optimal use, we recommend • For optimal use, we recommend: iPhone/iPad, rd iPhone 3GS, iPod Touch (3 s iPhone 3GS, iPod Touch (3rd Android, and generation), iPad iOS 4.0, or later generation), iPad iOS 4.0, or later • Download the MyItinerary app by s Most mobile devices using Android searching for “ScholarOne” in the BlackBerry! 2.2 or later with the default browser App Store directly from your mobile device. Or, access the link below or s y BlackBerr Torch or later device using scan the QR code to access the iTunes BlackBerry OS 7.0 with the default page for the app. http://itunes.apple. browser com/us/app/scholarone-my-itinerary/ • Download the MyItinerary app by id497884329?mt=8 scanning the QR code or accessing • Select the meeting “AIAA AVIATION http://download.abstractcentral.com/ 2013” aiaa-mav13/index.htm • Once downloaded, you can bookmark the site to access it later or add a link to your home screen. -
Aerodynamics and Aircraft Design
RESTRICTED AND AIRCRAFT DESIGN A REPORT PREPARED FOR THE AAF SCIENTIFIC ADVISORY GROUP By H. S. TSIEN Gllggenheim Laboratory California Institllte of Technology W. R. SEARS AND IRVING ASHKENAS Northrop Aircraft Company, Hawthorne, California C. N. HASERT Captain, Air Corps N. M. NEWMARK Talbot Laboratory Unif!ersity of Illinois • Pllblished MIIY, 1946 by HEADQUARTERS AIR MATERIEL COMMAND PUBLICATIONS BRANCH. INTELLIGENCE T-2 •• WRIGHT FIELD, DAYTON, OHIO RESTRICTED The AAF Scientific Advisory Group was activated late in 1944 by General of the Army H. H. Arnold. He se cured the services of Dr. Theodore von Karman, re nowned scientist and consultant in aeronautics, who agreed to organize and direct the group. Dr. von Karman gathered:wbout him a group of Ameri can scientists from every field of research having a bearing on air power. These men then analyzed im portant developments in the basic sciences, both here and abroad, and attempted to evaluate the effects of their application to air power. This volume is one of a group of reports made to the Army Air Forces by the Scientific Advisory Group. This document contains information affedlng the national defense of the United States within the meaning of the Espionage Act, SO U. S. C., 31 and 32, as amended. Its transmission or the revelation of its contents in any manner to an unauthorized person is prohibited by law. AA. SCIENTI.IC ADVISORY GROUP Dr. Th. von Karman Director Colonel F. E. Glantzberg Dr. H. L. Dryden Deputy Director, Military Deputy Director, Scientific Lt Col G. T. McHugh, Executive Capt C. H. -
Parametric Analysis of a Large-Scale Cycloidal Rotor in Hovering Conditions
Chalmers Publication Library Parametric Analysis of a Large-scale Cycloidal Rotor in Hovering Conditions This document has been downloaded from Chalmers Publication Library (CPL). It is the author´s version of a work that was accepted for publication in: Journal of Aerospace Engineering (ISSN: 0893-1321) Citation for the published paper: Xisto, C. ; Leger, J. ; Páscoa, J. et al. (2016) "Parametric Analysis of a Large-scale Cycloidal Rotor in Hovering Conditions". Journal of Aerospace Engineering http://dx.doi.org/10.1061/(ASCE)AS.1943- 5525.0000658 Downloaded from: http://publications.lib.chalmers.se/publication/235793 Notice: Changes introduced as a result of publishing processes such as copy-editing and formatting may not be reflected in this document. For a definitive version of this work, please refer to the published source. Please note that access to the published version might require a subscription. Chalmers Publication Library (CPL) offers the possibility of retrieving research publications produced at Chalmers University of Technology. It covers all types of publications: articles, dissertations, licentiate theses, masters theses, conference papers, reports etc. Since 2006 it is the official tool for Chalmers official publication statistics. To ensure that Chalmers research results are disseminated as widely as possible, an Open Access Policy has been adopted. The CPL service is administrated and maintained by Chalmers Library. (article starts on next page) PARAMETRIC ANALYSIS OF A LARGE-SCALE CYCLOIDAL ROTOR IN HOVERING CONDITIONS Carlos M. Xisto (corresponding author)1, J. A. Leger 2, J. C. P´ascoa 3, L. Gagnon4, P. Masarati 5, D. Angeli6 and A. Dumas 7 ABSTRACT In this work, four key design parameters of cycloidal rotors, namely the airfoil section; the number of blades; the chord-to-radius ratio; and the pitching axis location, are addressed. -
SBIR A02.07: VTOL to Transonic Aircraft
Acuity Technologies Proprietary SBIR A02.07: VTOL to Transonic Aircraft Final Technical Report July 24, 2006 Acuity Technologies Inc. Principal Investigator: Robert Clark 3475 Edison Way Unit P Menlo Park, CA 94025 650-369-6783 Issued by NASA Dryden Flight Research Center PO Box 273, Mailstop 1422 Edwards, California 93523-0273 Attn: Michelle L. Vial, (661) 276-3513 Contract No. NND06AA26C Effective Date: 1/26/2006 Technical Liaison Richard Maine 661-276-3316 [email protected] SBIR Rights Notice (Mar 1994) These SBIR data are furnished with SBIR rights under Contract No. NND06AA26C. For a period of 4 years after acceptance of all items to be delivered under this contract, the Government agrees to use these data for Government purposes only, and they shall not be disclosed outside the Government (including disclosure for procurement purposes) during such period without permission of the Contractor, except that, subject to the foregoing use and disclosure prohibitions, such data may be disclosed for use by support Contractors. After the aforesaid 4-year period the Government has a royalty-free license to use, and to authorize others to use on its behalf, these data for Government purposes, but is relieved of all disclosure prohibitions and assumes no liability for unauthorized use of these data by third parties. This Notice shall be affixed to any reproductions of these data, in whole or in part.” The views and conclusions contained in this document are those of the authors and should not be interpreted as representing the official policies, either express or implied, of NASA or the U.S. -
Personal Air Vehicle & VTOL
PERSPECTIVEPERSPECTIVE ARTICLE 21(69), July 1, 2014 ISSN 2278–5469 EISSN 2278–5450 Discovery Personal Air Vehicle & VTOL: An Insight Ravi Katukam҉ Convener Engineering Innovation, Cyient Limited, Hyderabad, India ҉Corresponding author: Convener Engineering Innovation, Cyient Limited, Hyderabad, India; Email: [email protected] Publication History Received: 06 May 2014 Accepted: 13 June 2014 Published: 1 July 2014 Citation Ravi Katukam. Personal Air Vehicle & VTOL: An Insight. Discovery, 2014, 21(69), 128-134 Publication License This work is licensed under a Creative Commons Attribution 4.0 International License. General Note Article is recommended to print as color digital version in recycled paper. ABSTRACT The rapid progress seen in the areas of Science and Technology have not resolved even some of our basic transportation issues. The challenges only seem to have increased with the passage of time. The ever increasing population coupled with the increasing trends of transportation requirements is pushing the scientists and the R&D engineers across the globe to invent and discover more efficient aircrafts which are not only eco-friendly but also provide a convenient and cost effective means of transportation of man and material. The evolution of Personal Air Vehicles (PAV) is expected to provide a possible solution for this problem. The design of the PAV was evolved from the appearance of a flightless bird named Puffin which is eco-friendly in nature and so, its structure is incorporated in the basic skeleton of the vehicles by few scientists. The striking appearance includes an unusual landing tail sitter which has its landing gear covered while it is in flight mode. -
Distribution Agreement in Presenting This Thesis As a Partial Fulfillment Of
Distribution Agreement In presenting this thesis as a partial fulfillment of the requirements for a degree from Emory University, I hereby grant to Emory University and its agents the non-exclusive license to archive, make accessible, and display my thesis in whole or in part in all forms of media, now or hereafter now, including display on the World Wide Web. I understand that I may select some access restrictions as part of the online submission of this thesis. I retain all ownership rights to the copyright of the thesis. I also retain the right to use in future works (such as articles or books) all or part of this thesis. Jeffrey C. Haylon April 10, 2018 Eyes Turned Skyward: Aviation, Myth, and Society in Germany, 1900-1933 by Jeffrey C. Haylon Dr. Astrid M. Eckert Adviser Department of History Dr. Astrid M. Eckert Adviser Dr. Patrick Allitt Committee Member Dr. Hiram Maxim Committee Member 2018 Eyes Turned Skyward: Aviation, Myth, and Society in Germany, 1900-1933 By Jeffrey C. Haylon Dr. Astrid M. Eckert Adviser An abstract of a thesis submitted to the Faculty of Emory College of Arts and Sciences of Emory University in partial fulfillment of the requirements of the degree of Bachelor of Arts with Honors Department of History 2018 Abstract Eyes Turned Skyward: Aviation, Myth, and Society in Germany, 1900-1933 By Jeffrey C. Haylon To the Germans of the early twentieth century, the development of aviation was not merely a technological endeavor but a social cause belonging to the entire nation. Beginning with the development of giant airships before the First World War, manned flight captivated the German people and the language surrounding it encapsulated contemporary social trends. -
Amphibious Aircrafts
Amphibious Aircrafts ...a short overview i Title: Amphibious Aircrafts Subtitle: ...a short overview Created on: 2010-06-11 09:48 (CET) Produced by: PediaPress GmbH, Boppstrasse 64, Mainz, Germany, http://pediapress.com/ The content within this book was generated collaboratively by volunteers. Please be advised that nothing found here has necessarily been reviewed by people with the expertise required to provide you with complete, accurate or reliable information. Some information in this book may be misleading or simply wrong. PediaPress does not guarantee the validity of the information found here. If you need specific advice (for example, medical, legal, financial, or risk management) please seek a professional who is licensed or knowledge- able in that area. Sources, licenses and contributors of the articles and images are listed in the section entitled ”References”. Parts of the books may be licensed under the GNU Free Documentation License. A copy of this license is included in the section entitled ”GNU Free Documentation License” All third-party trademarks used belong to their respective owners. collection id: pdf writer version: 0.9.3 mwlib version: 0.12.13 ii Contents Articles 1 Introduction 1 Amphibious aircraft . 1 Technical Aspects 5 Propeller.............................. 5 Turboprop ............................. 24 Wing configuration . 30 Lift-to-drag ratio . 44 Thrust . 47 Aircrafts 53 J2F Duck . 53 ShinMaywa US-1A . 59 LakeAircraft............................ 62 PBYCatalina............................ 65 KawanishiH6K .......................... 83 Appendix 87 References ............................. 87 Article Sources and Contributors . 91 Image Sources, Licenses and Contributors . 92 iii Article Licenses 97 Index 103 iv Introduction Amphibious aircraft Amphibious aircraft Canadair CL-415 operating on ”Fire watch” out of Red Lake, Ontario, c.