Auswahl der wissenschaftlichen Literatur zum Thema „Aeronautical assembly“
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Zeitschriftenartikel zum Thema "Aeronautical assembly"
Atik, Hafsa, Mouhssine Chahbouni, Driss Amagouz und Said Boutahari. „An analysis of springback of compliant assemblies by contact modeling and welding distortion“. International Journal of Engineering & Technology 7, Nr. 1 (27.01.2018): 85. http://dx.doi.org/10.14419/ijet.v7i1.8330.
Der volle Inhalt der QuelleDessena, Gabriele, Dmitry I. Ignatyev, James F. Whidborne, Alessandro Pontillo und Luca Zanotti Fragonara. „Ground Vibration Testing of a Flexible Wing: A Benchmark and Case Study“. Aerospace 9, Nr. 8 (10.08.2022): 438. http://dx.doi.org/10.3390/aerospace9080438.
Der volle Inhalt der Quelleda Silva, Bruno Jensen Virginio, Reinaldo Morabito, Denise Sato Yamashita und Horacio Hideki Yanasse. „Production scheduling of assembly fixtures in the aeronautical industry“. Computers & Industrial Engineering 67 (Januar 2014): 195–203. http://dx.doi.org/10.1016/j.cie.2013.11.009.
Der volle Inhalt der QuelleMei, Biao, Weidong Zhu, Pengyu Zheng und Yinglin Ke. „Variation modeling and analysis with interval approach for the assembly of compliant aeronautical structures“. Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture 233, Nr. 3 (06.02.2018): 948–59. http://dx.doi.org/10.1177/0954405418755823.
Der volle Inhalt der QuelleBorreguero-Sanchidrian, T. „Scheduling of an aeronautical final assembly line: a case study“. Procedia Manufacturing 13 (2017): 1167–74. http://dx.doi.org/10.1016/j.promfg.2017.09.179.
Der volle Inhalt der QuelleCheng, Hui, Yuan Li, Kai Fu Zhang und Feng Guo. „Deformation Analysis Method for Aeronautical Thin Walled Structures with Automated Riveting“. Applied Mechanics and Materials 271-272 (Dezember 2012): 1526–30. http://dx.doi.org/10.4028/www.scientific.net/amm.271-272.1526.
Der volle Inhalt der QuelleKortaberria, Gorka, Unai Mutilba, Jon Eguskiza und Joel Martins. „Simulation of an Aeronautical Product Assembly Process Driven by a Metrology Aided Virtual Approach“. Metrology 2, Nr. 4 (06.10.2022): 427–45. http://dx.doi.org/10.3390/metrology2040026.
Der volle Inhalt der QuelleBorreguero, T., F. Mas, J. L. Menéndez und M. A. Barreda. „Enhanced Assembly Line Balancing and Scheduling Methodology for the Aeronautical Industry“. Procedia Engineering 132 (2015): 990–97. http://dx.doi.org/10.1016/j.proeng.2015.12.587.
Der volle Inhalt der QuelleChang, Zhengping, Zhongqi Wang, Bo Jiang, Jinming Zhang, Feiyan Guo und Yonggang Kang. „Modeling and predicting of aeronautical thin-walled sheet metal parts riveting deformation“. Assembly Automation 36, Nr. 3 (01.08.2016): 295–307. http://dx.doi.org/10.1108/aa-10-2015-077.
Der volle Inhalt der QuelleGuo, Feiyan, Qingdong Xiao, Shihong Xiao und Zhongqi Wang. „Analysis on quantifiable and controllable assembly technology for aeronautical thin-walled structures“. Robotics and Computer-Integrated Manufacturing 80 (April 2023): 102473. http://dx.doi.org/10.1016/j.rcim.2022.102473.
Der volle Inhalt der QuelleDissertationen zum Thema "Aeronautical assembly"
Haoua, Abdoulaye affadine. „Smart Machining pour l’assemblage aéronautique“. Electronic Thesis or Diss., Paris, HESAM, 2023. http://www.theses.fr/2023HESAE090.
Der volle Inhalt der QuelleHybrid stacks comprising of composite CFRP layers, TA6V, and aluminum alloy, referred to as multi-material, are widely used in aerospace components. One-shot drilling, using an Automatic Drilling Unit (UPA), of these stacks poses major challenges due to the difference in machinability among the various materials within the stack. To meet quality requirements, improve tool life and achieve optimal productivity during the drilling of multi-material stacks with an electric UPA, it is essential to adapt cutting parameters during machining. However, there are currently no tools available to meet this need. This theisis conerns machine learning-based solutions for the implementation of smart drilling strategies incorporating adaptive machining. These solutions focus on the development of robust and reliable methodologies for identifying materials, detecting tool wear, and detecting multi-material drilling-related incidents (tool breakage, chip jamming, lubrication issues, cutting edges chipping). Fristly, a new approach to incident detection was proposed, based on unlabeled industrial data and clustering algorithms: K-means and hierarchical ascending classification. This approach enabled us to identify a number of incidents, and highlighted the difficulties associated with processing industrial data (rarity of incidents and absence of labels) and the difficulties associated with defining the optimum parameters for machine learning algorithms. Subsequently, experiment are performed on an specialized instrumented drilling bench and on Al7175/CFP and CFRP/Al7175 stacks. This led to the development and validation of an original material identification methodology based on Random Forest (RF). The results, in terms of material classification (Al7175, CFRP), enabled the extension of the RF model to different stack configurations with various tool diameters and a wide range of cutting conditions. This methodology will enable the implementation of an adaptive machining process on an electric UPA for multi-material drilling.Keywords : Adaptive drilling, Multi-material stacks drilling, Material recognition, Random Forest, Tool Wear, Unsupervised learning, Electric UPA, Signals analysis
Anderson, David Elliott. „Supervisory control algorithms for telerobotic space structure assembly“. Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/35941.
Der volle Inhalt der QuelleGralla, Erica Lynn. „Strategies for launch and assembly of modular spacecraft“. Thesis, Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/37886.
Der volle Inhalt der QuelleIncludes bibliographical references (p. 97-101).
NASA's human lunar and Mars exploration program requires a new transportation system between Earth and the Moon or Mars. In recent years, unfortunately, human space exploration programs have faced myriad political, technical, and financial difficulties. In order to avoid such problems, future human space exploration programs should be designed from the start for affordability. This thesis addresses one aspect of affordable exploration programs by tackling the issue of high costs for access to space. While launch vehicle trades for exploration programs are relatively well understood, on-orbit assembly has been given much less attention, but is an equally important component of the infrastructure enabling human access to space. Two separate but related perspectives on in-space assembly of modular spacecraft are provided: first, the coupling between launch vehicle selection, vehicle design, and on-orbit assembly is explored to provide a quantitative understanding of this combined tradespace; and second, a number of on-orbit assembly methods are analyzed in order to understand the potential value of a reusable assembly support infrastructure.
(cont.) Within the first topic, a quantitative enumeration of the launcher-assembly tradespace (in terms of both cost and risk) is provided based on a generalizable process for generating spacecraft modules and launch manifests from a transportation architecture. An optimal module size and launcher capability is found for a sample architecture at 82 metric tons; a 28-mt EELV emerges as another good option. The results show that the spacecraft design, assembly planning, and launcher selection are highly coupled and should be considered together, rather than separately. Within the second topic, four separate assembly strategies involving module self-assembly, tug-based assembly, and in-space refueling are modeled and compared in terms of mass-to-orbit requirements for various on-orbit assembly tasks. Results show that the assembly strategy has a significant impact on overall launch mass, and reusable space tugs with in-space refueling can significantly reduce the required launch mass for on-orbit assembly. This thesis thus examines a broad but focused set of issues associated with on-orbit assembly of next-generation modular spacecraft.
by Erica Lynn Gralla.
S.M.
Koonmen, James P. (James Patrick). „Implementing precision assembly techniques in the commercial aircraft industry“. Thesis, Massachusetts Institute of Technology, 1994. http://hdl.handle.net/1721.1/12120.
Der volle Inhalt der QuelleHedgecock, Judson C. „Implementation of distributed processing for the beam assembly teleoperator“. Thesis, Massachusetts Institute of Technology, 1990. http://hdl.handle.net/1721.1/43021.
Der volle Inhalt der QuelleKatz, Jacob G. „Estimation and control of flexible space structures for autonomous on-orbit assembly“. Thesis, Massachusetts Institute of Technology, 2009. http://hdl.handle.net/1721.1/50599.
Der volle Inhalt der QuelleIncludes bibliographical references (p. 135-139).
The ability to autonomously assemble large structures in space is desirable for the construction of large orbiting solar arrays, interplanetary spacecraft, or space telescopes. One technique uses free-flying satellites to manipulate and connect elements of the structure. Since these elements are often flexible and lack embedded actuators and sensors, the assembly robot must use its own actuators and onboard measurements to suppress vibrations during transportation maneuvers. This thesis will examine the dynamic modeling of a free-flying robot attached to a flexible beam-like element, vision-based estimation of vibrational motion, and trajectory control for assembly of a space structure.
by Jacob G. Katz.
S.M.
Bunn, Jason Chrisotopher. „Evaluation of assembly simulators used in closed loop attitude control system testing“. Thesis, Massachusetts Institute of Technology, 1997. http://hdl.handle.net/1721.1/47403.
Der volle Inhalt der QuelleMcCarthy, Bryan Patrick. „Flight hardware development for a space-based robotic assembly and servicing testbed“. Thesis, Massachusetts Institute of Technology, 2014. http://hdl.handle.net/1721.1/90780.
Der volle Inhalt der QuelleCataloged from PDF version of thesis. "This material is declared a work of the United States Government and is not subject to copyright protection in the United States."
Includes bibliographical references (pages 161-165).
Robotic assembly and servicing missions in space are becoming increasingly attractive for their potential to expand space capabilities and save money. Future missions may construct large systems on-orbit, service existing space assets, or remove retired satellites from valuable locations in the Geosynchronous orbit, among other things. Due to the high-risk nature of these missions, rigorous test facilities are a necessity. This thesis examines the existing testbeds for robotic assembly and servicing technologies and argues that a new, space-based testbed is necessary. It presents initial ground testing results for applicable control concepts, which also indicate that the dynamic authenticity associated with a six-degree-of-freedom on-orbit testbed is crucial for further development. This thesis then presents the requirements for such a testbed and describes the SPHERES Facility on the International Space Station. The facility, created by members of MIT's Space Systems Laboratory, has many of the desired testbed characteristics and can be easily expanded to meet the requirements through a hardware augmentation known as the Halo. The thesis develops the requirements for the Halo and then steps through the conception, design, and implementation of that hardware, along with the planned operations aboard the International Space Station.
by Bryan Patrick McCarthy.
S.M.
Jefferson, Thomas G. „Reconfigurable assembly system design methodology for aerospace wing structures“. Thesis, University of Nottingham, 2017. http://eprints.nottingham.ac.uk/42778/.
Der volle Inhalt der QuelleShah, Ankit Jayesh. „Planning for manipulation of interlinked deformable linear objects with applications to aircraft assembly“. Thesis, Massachusetts Institute of Technology, 2016. http://hdl.handle.net/1721.1/105640.
Der volle Inhalt der QuelleCataloged from PDF version of thesis.
Includes bibliographical references (pages 83-87).
Manipulation of deformable linear objects (DLO) has potential applications in the fields of aerospace and automotive assembly. In this paper, we introduce a problem formulation for attaching a set of interlinked DLOs to a support structure using a set of clamping points. The formulation describes the manipulation planning problem in terms of known clamping locations; pre-determined ideal clamping locations on the cables, called "reference points", and a set of finite gripping points on the DLOs. We also present a prototype algorithm that generates a solution in terms of primitive manipulation actions. The algorithm guarantees that no interlink constraints are violated at any stage of manipulation. We incorporate gravity in the computation of a DLO shape and propose a property linking geometrically similar cable shapes across the space of cable length and stiffness. This property allows for the computation of solutions for unit length and scaling of these solutions to appropriate length, potentially resulting in faster shape computation.
by Ankit Jayesh Shah.
S.M.
Bücher zum Thema "Aeronautical assembly"
Service, Iowa General Assembly Committee on Air. Committee on Air Service report to the General Assembly. s.l: Iowa Dept. of Transportation, 2000.
Den vollen Inhalt der Quelle findenCalifornia. Legislature. Assembly. Select Committee on Aviation. The state's role in aviation safety: Interim hearing conducted by Assembly Select Committee on Aviation, October 20, 1986, State Capitol, Sacramento, California. Sacramento, CA (Box 90, State Capitol, Sacramento 95814): Joint Publications Office, 1986.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Final test report for the qualification of the gristblast assembly and process for the inside diameter of the RSRM forward and aft domes. Brigham City, UT: Thiokol Corporation Space Operations, 1992.
Den vollen Inhalt der Quelle findenMeeting, COSPAR Plenary. Laboratory planetology: Proceedings of the B2 Symposium of COSPAR Scientific Commission B which was held during the Thirtieth COSPAR Scientific Assembly, Hamburg, Germany, 11-21 July, 1994. Oxford: Published for the Committee on Space Research [by] Pergamon, 1995.
Den vollen Inhalt der Quelle findenAssembly, COSPAR Scientific. Anticipating a solar probe: Proceedings of the D1.2 meeting of COSPAR Scientific Commission D, which was held during the thirtieth COSPAR Scientific Assembly, Hamburg, Germany, 11-21 July, 1994. Oxford, England: Published for the Committee on Space Research [by] Pergamon, 1995.
Den vollen Inhalt der Quelle findenOffice, General Accounting. Space station: Cost to operate after assembly is uncertain : report to Congressional requesters. Washington, D.C. (P.O. Box 37050, Washington, D.C. 20013): The Office, 1999.
Den vollen Inhalt der Quelle findenAssembly, COSPAR Scientific. Near-earth radiation environment including time variations and secondary radiation: Proceedings of the meetings of F2.6 and F2.7 of COSPAR Scientific Commission F, which was held during the thirtieth COSPAR Scientific Assembly, Hamburg, Germany, 11-21 July, 1994. Oxford, England: Published for the Committee on Space Research [by] Pergamon, 1995.
Den vollen Inhalt der Quelle findenCOSPAR. Panel on Technical Problems Related to Scientific Ballooning. PSB Meeting. Scientific ballooning: Proceedings of the PSB Meeting of the COSPAR Panel on Technical Problems Related to Scientific Ballooning which was held during the Thirtieth COSPAR Scientific Assembly, Hamburg, Germany, 11-21 July 1994. Oxford: Published for the Committee on Space Research [by] Pergamon, 1995.
Den vollen Inhalt der Quelle findenAssembly, COSPAR Scientific. Life and gravity: Physiological and morphological responses : proceedings of the F1.1 meeting of COSPAR Scientific Commission F, which was held during the thirtieth COSPAR Scientific Assembly, Hamburg, Germany, 11-21 July, 1994. Oxford, England: Published for the Committee on Space Research [by] Pergamon, 1995.
Den vollen Inhalt der Quelle findenVirginia. Dept. of State Police. Use of funds provided from the Rescue Assistance Fund for aviation (Med Flight) operations: Report of the Virginia Department of State Police to the Governor and the General Assembly of Virginia. Richmond, Va: Commonwealth of Virginia, 2005.
Den vollen Inhalt der Quelle findenBuchteile zum Thema "Aeronautical assembly"
Mozzillo, Rocco, Ferdinando Vitolo, Paola Iaccarino und Pasquale Franciosa. „Tolerance Prediction for Determinate Assembly Approach in Aeronautical Field“. In Lecture Notes in Mechanical Engineering, 229–40. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-31154-4_20.
Der volle Inhalt der QuelleGringoz, F., F. Thiébaut, C. Lartigue und B. Soufflet. „Free-State Shape of Aeronautical Components for Assembly Simulation“. In Advances on Mechanics, Design Engineering and Manufacturing II, 203–12. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-12346-8_20.
Der volle Inhalt der QuellePichon, Guillaume, Alain Daidie, Adeline Fau, Clément Chirol und Audrey Benaben. „Cold Working Process on Hard Metal Stacked Assembly“. In Lecture Notes in Mechanical Engineering, 41–47. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-70566-4_8.
Der volle Inhalt der QuelleMorales-Palma, Domingo, Ignacio Eguía, Manuel Oliva, Fernando Mas und Carpóforo Vallellano. „Managing Maturity States in a Collaborative Platform for the iDMU of Aeronautical Assembly Lines“. In Product Lifecycle Management and the Industry of the Future, 667–76. Cham: Springer International Publishing, 2017. http://dx.doi.org/10.1007/978-3-319-72905-3_59.
Der volle Inhalt der QuelleNuñez, Alex Aquieta, Anouck Chan, Alberto Donoso-Arciniega, Thomas Polacsek und Stéphanie Roussel. „A Collaborative Model for Connecting Product Design and Assembly Line Design: An Aeronautical Case“. In Lecture Notes in Business Information Processing, 267–80. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-91279-6_19.
Der volle Inhalt der QuelleMas, Fernando, Alejandro Gómez, José Luis Menéndez und José Ríos. „Proposal for the Conceptual Design of Aeronautical Final Assembly Lines Based on the Industrial Digital Mock-Up Concept“. In Product Lifecycle Management for Society, 10–19. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-41501-2_2.
Der volle Inhalt der QuelleCugini, Umberto. „Feature-Based Assembly for Aeronautics“. In CAD Tools and Algorithms for Product Design, 31–46. Berlin, Heidelberg: Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-04123-9_3.
Der volle Inhalt der QuelleTardieu, Hubert. „Role of Gaia-X in the European Data Space Ecosystem“. In Designing Data Spaces, 41–59. Cham: Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-93975-5_4.
Der volle Inhalt der QuelleCaggiano, Alessandra, Luigi Nele und Roberto Teti. „Drilling of Fiber-Reinforced Composite Materials for Aeronautical Assembly Processes“. In Characterizations of Some Composite Materials. IntechOpen, 2019. http://dx.doi.org/10.5772/intechopen.80466.
Der volle Inhalt der QuelleMegnafi, Hicham, und Walid Yassine Medjati. „Quadrotor-Type UAVs Assembly and Its Application to Audit Telecommunications Relays“. In Aeronautics - New Advances. IntechOpen, 2022. http://dx.doi.org/10.5772/intechopen.104254.
Der volle Inhalt der QuelleKonferenzberichte zum Thema "Aeronautical assembly"
Da Costa, Sylvain J. „FACAI - A Flexible Assembly Cell for Aeronautical Industry“. In Aerofast Conference & Exposition. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 1993. http://dx.doi.org/10.4271/931770.
Der volle Inhalt der QuelleLeila, Troudi, und Jelassi Khaled. „Assembly defect detection using rivets in aeronautical structures“. In 2021 18th International Multi-Conference on Systems, Signals & Devices (SSD). IEEE, 2021. http://dx.doi.org/10.1109/ssd52085.2021.9429521.
Der volle Inhalt der QuelleHosokawa, Keisuke, Susumu Saito, Jun Sakai, Ichiro Tomizawa, Hiroyuki Nakata, Toru Takahashi, Michi Nishioka et al. „Observations of sporadic E using aeronautical navigation radio waves“. In XXXVth URSI General Assembly and Scientific Symposium. Gent, Belgium: URSI – International Union of Radio Science, 2023. http://dx.doi.org/10.46620/ursigass.2023.1493.mhft6662.
Der volle Inhalt der QuelleSaito, Susumu, Maho Nakamura, Takayuki Yoshihara, Minh Le Huy, Thang Nguyen Chien, Slamet Supriadi, Prayitno Abadi und Dwiko Unggul Prabowo. „Characterization of Ionospheric Spatial Decorrelation for GNSS-based Aeronautical Navigation Systems“. In XXXVth URSI General Assembly and Scientific Symposium. Gent, Belgium: URSI – International Union of Radio Science, 2023. http://dx.doi.org/10.46620/ursigass.2023.2042.rwcc5650.
Der volle Inhalt der QuelleTabuchi, Shumpei, Keisuke Hosokawa, Susumu Saito, Jun Sakai, Ichiro Tomizawa, Toru Takahashi und Hiroyuki Nakata. „Observation of sporadic E using aeronautical navigation radio for instrument landing system“. In XXXVth URSI General Assembly and Scientific Symposium. Gent, Belgium: URSI – International Union of Radio Science, 2023. http://dx.doi.org/10.46620/ursigass.2023.1618.vfqi6822.
Der volle Inhalt der QuelleBordegoni, Monica, und Umberto Cugini. „Feature-Based Assembly Design: Concepts and Design Environment“. In ASME 1997 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/detc97/cie-4266.
Der volle Inhalt der QuelleMozzillo, Rocco, Paola Iaccarino, Ferdinando Vitolo und Pasquale Franciosa. „Design and development of jigless assembly process: the case of complex aeronautical systems“. In 2019 II Workshop on Metrology for Industry 4.0 and IoT (MetroInd4.0&IoT). IEEE, 2019. http://dx.doi.org/10.1109/metroi4.2019.8792874.
Der volle Inhalt der QuelleLourenco, E. J., M. Oliva, M. A. Estrela und A. J. Baptista. „Multidimensional Design Assessment Model for eco-efficiency and efficiency in aeronautical assembly processes“. In 2019 IEEE International Conference on Engineering, Technology and Innovation (ICE/ITMC). IEEE, 2019. http://dx.doi.org/10.1109/ice.2019.8792641.
Der volle Inhalt der QuelleOtto, A. J., R. P. Millenaar, C. Van der Merwe, T. Abbott, S. Tshongweni und A. R. Botha. „Aeronautical radio frequency interference characterisation for the square kilometre array“. In 2017 XXXIInd General Assembly and Scientific Symposium of the International Union of Radio Science (URSI GASS). IEEE, 2017. http://dx.doi.org/10.23919/ursigass.2017.8104497.
Der volle Inhalt der QuelleLin, Jia, Sun Jin, Cheng Zheng, Fuyong Yang und Siyi Ding. „Variation Analysis of Accumulative Stresses in Multistep Assembly Processes Using Output Transformation Matrices“. In ASME 2017 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/imece2017-71215.
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