Academic literature on the topic 'Aerospace systems design'
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Journal articles on the topic "Aerospace systems design"
Valenti, Michael. "Re-Engineering Aerospace Design." Mechanical Engineering 120, no. 01 (January 1, 1998): 70–72. http://dx.doi.org/10.1115/1.1998-jan-5.
Full textSira-Ramirez, H., P. Lischinsky-Arenas, and O. Llanes-Santiago. "Dynamic compensator design in nonlinear aerospace systems." IEEE Transactions on Aerospace and Electronic Systems 29, no. 2 (April 1993): 364–79. http://dx.doi.org/10.1109/7.210075.
Full textLivne, Eli. "Special Issue: Multidisciplinary Design Optimization of Aerospace Systems." Journal of Aircraft 36, no. 1 (January 1999): 9–10. http://dx.doi.org/10.2514/2.2439.
Full textMonell, Donald W., and William M. Piland. "Aerospace systems design in NASA's collaborative engineering environment." Acta Astronautica 47, no. 2-9 (July 2000): 255–64. http://dx.doi.org/10.1016/s0094-5765(00)00065-5.
Full textWang, Yi Wen, Ming Na Ding, Wen Juan Zheng, Zhen Chen, and Jing Shu Hu. "Design of Typical Aerospace Materials Database System." Materials Science Forum 800-801 (July 2014): 644–48. http://dx.doi.org/10.4028/www.scientific.net/msf.800-801.644.
Full textShi, Renhe, Teng Long, Nianhui Ye, Yufei Wu, Zhao Wei, and Zhenyu Liu. "Metamodel-based multidisciplinary design optimization methods for aerospace system." Astrodynamics 5, no. 3 (September 2021): 185–215. http://dx.doi.org/10.1007/s42064-021-0109-x.
Full textGil, Paulo J. S., Pedro M. B. Rosa, and Ivo M. L. Ferreira. "Modern approaches in the design of complex aerospace systems." Journal of Aerospace Engineering, Sciences and Applications 2, no. 1 (January 1, 2010): 15–26. http://dx.doi.org/10.7446/jaesa.0201.02.
Full textBindolino, G., S. Ricci, and P. Mantegazza. "Integrated Servostructural Optimization in the Design of Aerospace Systems." Journal of Aircraft 36, no. 1 (January 1999): 167–75. http://dx.doi.org/10.2514/2.2423.
Full textGupta, K. K. "An Integrated Systems Approach for Design of Aerospace Structures." International Journal of Space Structures 3, no. 2 (June 1988): 118–29. http://dx.doi.org/10.1177/026635118800300205.
Full textSaleh, Joseph H., Daniel E. Hastings, and Dava J. Newman. "Flexibility in system design and implications for aerospace systems." Acta Astronautica 53, no. 12 (December 2003): 927–44. http://dx.doi.org/10.1016/s0094-5765(02)00241-2.
Full textDissertations / Theses on the topic "Aerospace systems design"
Pfaender, Jens Holger. "Competitive Assessment of Aerospace Systems using System Dynamics." Diss., Georgia Institute of Technology, 2006. http://hdl.handle.net/1853/14014.
Full textFernandez, Martin Ismael. "Valuation of design adaptability in aerospace systems." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2008. http://hdl.handle.net/1853/22584.
Full textCommittee Chair: Dr. Mavris, Dimitri; Committee Member: Dr. Hollingsworth, Peter; Committee Member: Dr. McMichael, Jim; Committee Member: Dr. Saleh, Joseph; Committee Member: Dr. Schrage, Daniel.
Waslander, Steven L. "Multi-agent systems design for aerospace applications /." May be available electronically:, 2007. http://proquest.umi.com/login?COPT=REJTPTU1MTUmSU5UPTAmVkVSPTI=&clientId=12498.
Full textBorer, Nicholas Keith. "Decision Making Strategies for Probabilistic Aerospace Systems Design." Diss., Georgia Institute of Technology, 2006. http://hdl.handle.net/1853/10469.
Full textWang, Jennifer Y. "Migration of aerospace technologies to adjacent markets." Thesis, Massachusetts Institute of Technology, 2014. http://hdl.handle.net/1721.1/105302.
Full textCataloged from PDF version of thesis.
Includes bibliographical references (pages 51-56).
Shrinking government budgets due to economic woes has aerospace and defense contractors scrambling to sustain their business and minimize the effects of budget sequestration. Given the global economic climate and the level of federal debt, government budget spending is unlikely to recover in the near future to previous levels, where aerospace and defense contractors had enjoyed an abundance of million and billion dollar cost-reimbursable contracts. In current business conditions, company leadership has put a new focus on finding and developing business in adjacent markets, where core competencies can be utilized to generate alternative streams of revenue. In order to provide insight into potential adjacent markets for aerospace technologies and entry strategies that increase chances of success, this thesis analyzes cases of technologies originally developed for an aerospace application that were eventually adopted for use in another (non-aerospace) industry. Analysis of metrics and 35 cases compiled from NASA's Spinoff and Technology Databases reinforce several observations that have been generalized in other literature: 1) a wide variety of industries could be considered adjacent markets, 2) entering established industries may offer the highest technology adoption rate, 3) partnership with an existing firm or organization with knowledge of the adjacent market has played a key role in the successful adoption of the technology in the adjacent market, and 4) building-block technologies at the subsystem, component and base material level most often traversed market boundaries. However, a handful of cases prove that systems can traverse market boundaries in whole under certain conditions. Most importantly, the role of the aerospace industry as advanced analog lead users is a unique advantage that aerospace firms should leverage.
by Jennifer Y. Wang.
S.M. in Engineering and Management
Hart, Peter Bartholomew. "A plm implementation for aerospace systems engineering-conceptual rotorcraft design." Thesis, Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/28278.
Full textAgte, Jeremy S. (Jeremy Sundermeyer). "Multistate analysis and design : case studies in aerospace design and long endurance systems." Thesis, Massachusetts Institute of Technology, 2011. http://hdl.handle.net/1721.1/68167.
Full textThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.
"September 2011." Cataloged from student submitted PDF version of thesis.
Includes bibliographical references (p. 221-230).
This research contributes to the field of aerospace engineering by proposing and demonstrating an integrated process for the early-stage, multistate design of aerospace systems. The process takes into early consideration the many partially degraded states that real-world systems experience throughout their operation. Despite advancing efforts aimed at maintaining operation in a state of optimum performance, most systems spend very substantial amounts of time operating in degraded or off-nominal states (e.g. Hubble space telescope, Mars Spirit rover, or aircraft flying under minimum-equipment-list restrictions). There exist relatively few methods and tools to address this at the beginning of the design process. At one end of the spectrum is design optimization, but this typically concentrates on the system in its nominal state of operation, only infrequently considering failure states through piecemeal application of constraints. There is reliability analysis, which focuses on component failure rates and the benefits of redundancy but does not consider how well or poorly the system performs with partial failures. Finally, there is controls theory, where control laws are optimized but the plant is typically assumed to be given a priori. The methodology described within this thesis coordinates elements from each of these three areas into an effective integrated framework. It allows the designer deeper insight into the complex problem of designing cost effective systems that must operate for long durations with little or expensive opportunity for repair or intervention. Specific contributions include: 1) the above methodology, which evaluates responses in system expected performance and availability to changes in static design variables (geometry) and component failure rates, accounting for control design variables (gains) where appropriate, 2) the demonstration of the cost and benefits associated with a multistate design approach as compared to reliability analysis and the nominal design approach, and 3) a multilayer extension of Markov analysis, for translating single sortie vehicle level metrics into measures of multistate campaign performance. The process is demonstrated through three application case studies. The first of these establishes the feasibility of the approach through the multistate analysis of performance for an existing twin-engine aircraft. This analysis was enabled through the development of a multidisciplinary simulation based design model for evaluation of multistate aircraft performance. A medium-altitude long endurance unmanned aerial vehicle is designed in the second case study, first from a single-sortie, ultra long endurance perspective and then from a multiple sortie, mission campaign perspective. Finally, the third case study demonstrates applicability of the approach to a lower level subsystem, that of the lubrication system for a geared turbofan engine. Several major findings result from these case studies, including that: 1) multistate performance output spaces have distinctly unique shapes and boundaries, depending on whether formed through variation of component failure rates, static design variables (geometry), or a multistate combination of both, 2) a region of multistate performance results from the combined variation of failure rates and static design variables that is unachievable through the independent variation of either one, 3) small changes in static design variables may be used to significantly improve system availability, and 4) the general multistate design problem is one of competing objectives between system availability, expected performance, nominal performance, and cost.
by Jeremy S. Agte.
Ph.D.
Hollingsworth, Peter Michael. "Requirements Controlled Design: A Method for Discovery of Discontinuous System Boundaries in the Requirements Hyperspace." Diss., Available online, Georgia Institute of Technology, 2004:, 2004. http://etd.gatech.edu/theses/available/etd-04092004-151914/unrestricted/hollingsworth%5Fpeter%5Fm%5F200405%5Fphd.pdf.
Full textNickol, Craig, Committee Member ; Goodman, Seymour, Committee Member ; Schrage, Daniel, Committee Member ; Craig, James, Committee Member ; Mavris, Dimitri, Committee Chair. Vita. Includes bibliographical references (leaves 272-283).
Papageorgiou, George. "Robust control system design : H∞ loop sharing and aerospace applications." Thesis, University of Cambridge, 1998. https://www.repository.cam.ac.uk/handle/1810/272494.
Full textDaberkow, Debora Daniela. "A formulation of metamodel implementation processes for complex systems design." Diss., Georgia Institute of Technology, 2002. http://hdl.handle.net/1853/12478.
Full textBooks on the topic "Aerospace systems design"
Kumar, S. Kishore, Indira Narayanaswamy, and V. Ramesh, eds. Design and Development of Aerospace Vehicles and Propulsion Systems. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-15-9601-8.
Full textAlbers, James A. NASA Ames Aerospace Systems Directorate research. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1991.
Find full textKodiyalam, S. Multidisciplinary aerospace systems optimization, computational aerosciences (CAS) project. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.
Find full textEngineers, Society of Automotive, ed. Aerospace environmental systems: Proceedings of the Sixteenth ICES conference. Warrendale, PA: Society of Automotive Engineers, 1986.
Find full textBement, Laurence J. A manual for pyrotechnic design, development and qualification. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Find full textMishkin, A. H. Space-based multifunctional end effector systems: Functional requirements and proposed designs. Pasadena, Calif: National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology, 1988.
Find full textVoigt, Robert G. Requirements for multidisciplinary design of aerospace vehicles on high performance computers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Find full textMalone, J. B. The design of future airbreathing engine systems within an intelligent synthesis environment. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textMalone, J. B. The design of future airbreathing engine systems within an intelligent synthesis environment. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textConcurrent Design and Manufacture of Aerospace Transmission Systems (Conference) (1998 Derby (England)). Aerospace transmission systems: Concurrent design and manufacture : 20 May 1998, Rolls-Royce, Derby, UK. Bury St. Edmunds: Professional Engineering, 1998.
Find full textBook chapters on the topic "Aerospace systems design"
Perrotin, Maxime, Julien Delange, and Jérôme Hugues. "The Design of Aerospace Systems." In Distributed Systems, 191–227. Hoboken, NJ, USA: John Wiley & Sons, Inc., 2013. http://dx.doi.org/10.1002/9781118601365.ch9.
Full textBozzano, Marco, Harold Bruintjes, Alessandro Cimatti, Joost-Pieter Katoen, Thomas Noll, and Stefano Tonetta. "Formal Methods for Aerospace Systems." In Cyber-Physical System Design from an Architecture Analysis Viewpoint, 133–59. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4436-6_6.
Full textVassev, Emil, and Mike Hinchey. "Fundamentals of Designing Complex Aerospace Software Systems." In Complex Systems Design & Management, 65–80. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-25203-7_4.
Full textMinisci, Edmondo, and Massimiliano Vasile. "Multidisciplinary Design Optimization of Aerospace Transportation Systems." In Computational Intelligence in Aerospace Sciences, 491–528. Reston, VA: American Institute of Aeronautics and Astronautics, Inc., 2014. http://dx.doi.org/10.2514/5.9781624102714.0491.0528.
Full textPeriaux, Jacques, Felipe Gonzalez, and Dong Seop Chris Lee. "Multidisciplinary Design Optimisation and Robust Design in Aerospace Systems." In Intelligent Systems, Control and Automation: Science and Engineering, 53–68. Dordrecht: Springer Netherlands, 2015. http://dx.doi.org/10.1007/978-94-017-9520-3_5.
Full textGery, Eran. "Realizing Digital Systems Engineering—Aerospace and Defence Use Case." In Complex Systems Design & Management, 385–400. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-73539-5_29.
Full textSaadat, Mozafar. "Challenges in the Assembly of Large Aerospace Components." In Integrated Systems, Design and Technology 2010, 37–46. Berlin, Heidelberg: Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-17384-4_4.
Full textMartins, Joaquim R. R. A. "Chapter 19: Multidisciplinary Design Optimization of Aerospace Systems." In Advances and Trends in Optimization with Engineering Applications, 249–57. Philadelphia, PA: Society for Industrial and Applied Mathematics, 2017. http://dx.doi.org/10.1137/1.9781611974683.ch19.
Full textMavris, Dimitri N., and Olivia J. Pinon. "An Overview of Design Challenges and Methods in Aerospace Engineering." In Complex Systems Design & Management, 1–25. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-25203-7_1.
Full textRamalingam, Thirunavukkarasu, Joel Otto, and Benaroya Christophe. "Design Space Exploration for Aerospace IoT Products." In Re-imagining Diffusion and Adoption of Information Technology and Systems: A Continuing Conversation, 707–21. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-64849-7_62.
Full textConference papers on the topic "Aerospace systems design"
CHAMIS, C., and S. SINGHAL. "Computational simulation of concurrent engineering for aerospace propulsion systems." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1144.
Full textBecz, Sandor, Alessandro Pinto, Lawrence Zeidner, Ritest Khire, Hayden Reeve, and Andrzej Banaszuk. "Design System for Managing Complexity in Aerospace Systems." In 10th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-9223.
Full textWOLF, DIETER. "Transys - A software system for preliminary design, analysis and evaluation of space transportation systems." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1193.
Full textRYAN, ROBERT, and V. I. VERDERAIME. "Launch Vehicle Systems Design Analysis." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-1140.
Full textPETERSEN, T., and P. SUTCLIFFE. "Systems engineering as applied to the Boeing 777." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1010.
Full textBACKES, PAUL, MARK LONG, and ROBERT STEELE. "Designing minimal space telerobotics systems for maximum performance." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1015.
Full textBRIGGS, HUGH. "Integrated modeling and design of advanced optical systems." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1249.
Full textBraun, Robert, Ilan Kroo, and Peter Gage. "Post-optimality analysis in aerospace vehicle design." In Aircraft Design, Systems, and Operations Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3932.
Full textDECKER, D., L. INOUYE, and D. ROLANDELLI. "Design of hi-power unit components for space systems." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1062.
Full textSCHROEDER, W., R. BROGDON, J. PETERS, and C. GLANCY. "Application of RDD-100 for Space Station systems engineering." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1257.
Full textReports on the topic "Aerospace systems design"
Burns, John A. A Computational Environment for Design of Aerospace Systems. Fort Belvoir, VA: Defense Technical Information Center, April 2000. http://dx.doi.org/10.21236/ada379978.
Full textTeel, Andrew R. Hybrid Control Systems: Design and Analysis for Aerospace Applications. Fort Belvoir, VA: Defense Technical Information Center, February 2009. http://dx.doi.org/10.21236/ada495350.
Full textBurns, John A. Sensitivity and Adjoint Methods for Design of Aerospace Systems. Fort Belvoir, VA: Defense Technical Information Center, July 2002. http://dx.doi.org/10.21236/ada417179.
Full textJameson, Anthony, and Juan J. Alonso. Computational Algorithms for High-Fidelity Multidisciplinary Design of Complex Aerospace Systems. Fort Belvoir, VA: Defense Technical Information Center, December 2003. http://dx.doi.org/10.21236/ada430007.
Full textHaddad, Wassim M. An Energy-Based Thermodynamic Stabilization Framework for Hybrid Control Design of Large-Scale Aerospace Systems. Fort Belvoir, VA: Defense Technical Information Center, February 2009. http://dx.doi.org/10.21236/ada500028.
Full textRoye, Thorsten. The Right Level of Automation for Industry 4.0. SAE International, May 2022. http://dx.doi.org/10.4271/epr2022013.
Full text