Relevant bibliographies by topics / Design Space Analysis

Academic literature on the topic 'Design Space Analysis'

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Published: 10 December 2022
Last updated: 28 January 2023

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Journal articles on the topic "Design Space Analysis"

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李, 雅静. "Design Analysis of White Space Technique in Interior Space." Design 05, no. 01 (2020): 1–4. http://dx.doi.org/10.12677/design.2020.51001.

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Hanim Awang, Arita, and Zuraini Denan. "Designer’s Office in Malaysia: Comparative Analysis on Space Planning and Design Issues." International Journal of Social Science and Humanity 6, no. 6 (June 2016): 427–32. http://dx.doi.org/10.7763/ijssh.2016.v6.685.

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Ortiz, Joshua, Joshua Summers, James Coykendall, Travis Roberts, and Rahul Rai. "A TOPOLOGICAL FORMALISM FOR QUANTITATIVE ANALYSIS OF DESIGN SPACES." Proceedings of the Design Society 1 (July 27, 2021): 293–302. http://dx.doi.org/10.1017/pds.2021.30.

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AbstractThe objective of this paper is to present a mathematically grounded description of the two topological spaces for the design problem and the design solution. These spaces are derived in a generalized form such that they can be applied by researchers studying engineering design and developing new methods or engineers seeking to understand the influence that changes in the problem space have on the solution space. In addition to the formal definitions of the spaces, including assumptions and limitations, three types of supported reasoning are presented to demonstrate the potential uses. These include similarity analysis to compare spaces, an approach to sensitivity analysis of the solution space to changes in the problem space, and finally a distance measure to determine how far a current proposal is to the feasible solution space. This paper is presented to establish a common vocabulary for researchers when discussing, studying, and supporting the dyadic nature of engineering design (problem-solution co-evolution).
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Ji, Zhiming. "Analysis of Design Parameters in Platform Manipulators." Journal of Mechanical Design 118, no. 4 (December 1, 1996): 526–31. http://dx.doi.org/10.1115/1.2826923.

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Multi-loop parallel structures of platform manipulators present challenge to their design analysis. For studying the workspace of the 3-6 class of platforms, we developed the “vertex space” concept in Ji (1994). This paper extends the “vertex space,” concept to other structures for analysing and comparing their workspaces. We classify the vertices of the platform manipulators into types A and B. The platform manipulators are then divided into four groups based on their vertex types. Design parameters in platform manipulators are studied in terms of their functions and effects to vertex spaces and workspace.
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Masin, Michael, Lior Limonad, Aviad Sela, David Boaz, Lev Greenberg, Nir Mashkif, and Ran Rinat. "Pluggable Analysis Viewpoints for Design Space Exploration." Procedia Computer Science 16 (2013): 226–35. http://dx.doi.org/10.1016/j.procs.2013.01.024.

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Coffeen, Jeremy, Frederic Jacquelin, Richard Kepple, Rock Mendenhall, Michael Rodgers, Nicholas Roth, Richard Thompson, Richard Wise, and Roger Wong. "Georgia Aquarium Design Space Analysis and Optimization." Procedia Computer Science 44 (2015): 125–34. http://dx.doi.org/10.1016/j.procs.2015.03.001.

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McKerlie, Diane, and Allan MacLean. "Reasoning with Design Rationale: practical experience with design space analysis." Design Studies 15, no. 2 (April 1994): 214–26. http://dx.doi.org/10.1016/0142-694x(94)90026-4.

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Brown, Gary L. "DESIGN ANALYSIS CYCLE APPLICATION TO THE INTERNATIONAL SPACE STATION DESIGN." INCOSE International Symposium 6, no. 1 (July 1996): 52–54. http://dx.doi.org/10.1002/j.2334-5837.1996.tb01982.x.

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Kim, Il Yong, and Byung Man Kwak. "Design space optimization using a numerical design continuation method." International Journal for Numerical Methods in Engineering 53, no. 8 (2002): 1979–2002. http://dx.doi.org/10.1002/nme.369.

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Gao, Changzheng, Juepin Hou, Yanchen Ma, and Jianxin Yang. "Evaluation and Analysis of Design Elements for Sustainable Renewal of Urban Vulnerable Spaces." International Journal of Environmental Research and Public Health 19, no. 24 (December 9, 2022): 16562. http://dx.doi.org/10.3390/ijerph192416562.

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The sustainable renewal design of urban vulnerable spaces is critical for urban space quality improvement. Taking Zhengzhou and surrounding cities as examples, a cognitive framework of urban vulnerable spaces is constructed. The three types of urban vulnerable spaces are vulnerable population, vulnerable cultural, and vulnerable forgotten spaces. Their sustainable renewal design elements comprise multidimensional factors, such as functional requirement, space organization, activity facility, urban context continuation, and material texture. The design elements for the sustainable update of urban vulnerable spaces are evaluated by grey relation analysis (GRA), and update strategies are proposed. The result shows that (1) vulnerable population spaces were shown to have the highest sensitivity to functional requirements and activity facility design elements, while vulnerable cultural spaces have high relevance to urban context continuation and functional requirement design elements. Furthermore, space organization, activity facility, and urban context continuation design elements all show high relevance and importance in vulnerable forgotten spaces. (2) The update of vulnerable population spaces should be designed to achieve functional communion; vulnerable cultural spaces can be reshaped through urban context implantation, and vulnerable forgotten spaces can use space creation to enhance ecological space continuity, achieving sustainable renewal. The study provides a reference for decision-making for improving urban vulnerable habitats and the sustainable renewal design of atypical urban space types.
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Dissertations / Theses on the topic "Design Space Analysis"

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Puri, Manpreet Singh. "Design and analysis of inflatable space structures." Thesis, University of Strathclyde, 2016. http://digitool.lib.strath.ac.uk:80/R/?func=dbin-jump-full&object_id=28497.

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This thesis gives the conceptualization of inflation of inflatable membrane space structures. Although there has been little study using software simulation and the majority of documented research is based on theoretical numerical calculations. This research advanced the prior understanding of wrinkling within inflated membranes by using complex structures subjected to deformation loads. Within this thesis, a computational framework for the numerical analysis of the interaction between acting forces on the membrane and the membrane structure dynamics is presented. Moreover, in the case with thin membrane deformations, the synergy between the membrane wrinkling and structural forces has to be examined. This membrane structure-anatomical forces correlation results in a dynamic wrinkling problem, which can only be modelled easily and effectively by a simulation software that can integrate each assumption and attribute within the analysis. In the structural simulation within Abaqus FEA software, key consideration has to be given in modelling the geometric non-linearity behaviour of the membrane. By using the existing continuum expression for the virtual internal work in curvilinear coordinates. This is used to derive the modified fundamental formulation in which all subsequent analysis is established on and the initial equilibrium shape of the membrane. A critical feature of the new formulation is the prospect of adding pre-stressed forces to the membrane structure. The approach developed, established on an alteration of the material stiffness matrix to integrate the effects of wrinkling and deformation, can be utilized to calculate the behaviour of the membrane within a finite element simulation. In the wrinkling model, the state of the membrane element (taut, wrinkled or slack) is characterized by a mixed wrinkling criterion. Once it has been identified that the membrane element is wrinkled, an iterative scheme looks for the wrinkled orientation angle and the precise stress distribution, including only uni-axial tension in the wrinkle direction, is then derived. The wrinkling model has been verified and validated by contrasting the simulated conclusions with documented results for the instance of a time-independent isotropic membrane subjected to shear and axial loading. Utilizing the time integration method, a time-dependant pseudo-elastic stiffness matrix was represented and therefore, rather than calculating the convolution integral all through the Abaqus simulation, then we can calculate the behaviour of a membrane structure by superposition of a series of step by step increments in basic finite element software. The theoretical computations from the Abaqus/Explicit analysis were compared with documented results for the shear and axial loading. The results agreed very well, assuming friction and any relativistic dynamic effects were excluded. The discrepancy between the shear loading solution is 7% while the discrepancy between the axial loading is only 5% between the Abaqus modeland the documented model. This discrepancy could be the resultant of the source of energy dissipation from the visco-elastic behaviour during the loading and unloading of forces. It can be stated that for the Kapton HN membrane, this result falls within acceptable range but to increase accuracy, the load and unloading will be carried out on a set steady amplitude to inhibit in shock effects within the model. A three-dimensional finite element model which integrates wrinkling and frictionless contact has been developed to simulate the adaptive smart cell and cylindrical membrane structure. The loading of both structures is given by a non-uniform differential inflation pressure with a continual gradient adjacent to height. The resultant solutions are computed using Abaqus/Explicit software, with an integrated user-defined material subroutine to account for elastic wrinkling deformation that administers a combined stress-strain criterion. Frictionless contact within the membrane structure is prescribed for both complex structures (Adaptive Smart Structures Model and Inflatable Beam Model) in order to prohibit the penetration of the membrane structure through itself. Both the complex inflatable membrane wrinkling models accomplish the purpose of exceptional subgrid scale performance in relation to accuracy, competency, computing hardware & software expense, complexity and the model convergence rate. The numerical algorithm is created in general context and is flexible for a large variety of material models. For a closed membrane structure, the skew symmetric constraint parameters vanish, while the existing symmetric domain variables mirror preservation of the system. This procedure does not demand the discretization of the fluid (gas) domain or the link between coupling of fluid (gas) and membrane. As a result of this basic fact, the computation is drastically simplified. The adaptive structures model introduces a novel approach in harnessing solar power for reuse on the ground as a stable source of power. The simulations were based on the space part of the stiff structure created of hexagonal membrane cells. Simulations are carried out in Abaqus Finite Element Analysis software for simplicity & a comparison for validation purposes is tested against an experimental inflatable cell within a vacuum chamber. It was showcased that the final configuration could be achieved regardless of the packaging shape of the inflatable cell array. The inflatable beam model is comprised of two sections, the bending & buckling of the inflated beam and the post-inflation of the bent and buckled beam. Abaqus software was used to simulate the inflatable beam during each configuration utilizing the integration of a modified VUMAT subroutine. A comparison is showcased representing the importance of the integration of the VUMAT subroutine within our Abaqus model.
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Faedi, Alberto. "Design and Analysis of Optical Links for Space Communications." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2021. http://amslaurea.unibo.it/22859/.

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Studio e presentazione di link ottici in ambiente deep-space. Implementazione di simulatori in C++ relativi a due diverse tecniche di modulazione e demodulazione. Studio del link budget tra un satellite relay in orbita attorno alla Terra e un satellite in orbita attorno a pianeti solari (Venere, Marte, Urano e Nettuno). Studio e ricerca sul problema del puntamento in ambito ottico, per collegamenti deep-space.
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Lacroix, Frédéric 1973. "Design, analysis and implementation of free-space optical interconnects." Thesis, McGill University, 2001. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=38072.

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Optical interconnects represent an attractive alternative technology for the implementation of dense, high-speed interconnects, as they do not suffer from many of the problems plaguing electrical interconnects such as frequency-dependent crosstalk and attenuation.
However, optics has still not been accepted commercially as an interconnect technology. There is concern regarding the cost and complexity of the optomechanics needed to achieve the very fine alignments necessary to guarantee that the light emitted from the source actually falls on the receiver. The demonstration of a simple-to-assemble, dense and robust optical interconnect would constitute an important proof of the practicality of this technology. The photonic backplane demonstrator system presented in this thesis addresses these issues through a novel approach; the system uses slow Gaussian beams (f/16) and a clustered design to maximize misalignment tolerances. This in turn relaxes the positioning and packaging requirements for the components, thus simplifying assembly.
This thesis pursues two sets of complementary goals; the first set is concerned with the demonstration of some desirable optomechanical characteristics for optical interconnects such as passive alignment, repeatability and stability while the second set of goals is concerned with a verification of hypotheses often used in the design and implementation of optical interconnects. Such hypotheses are often used in practice to design optical interconnects despite the fact that little data exists in the literature to warrant their use. It therefore makes good sense to spend some time verifying the accuracy of these models. This will provide a solid engineering foundation for the design of future systems.
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Rising, John M. (John Michael). "Safety-guided design & analysis of space launch vehicles." Thesis, Massachusetts Institute of Technology, 2018. http://hdl.handle.net/1721.1/118525.

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Thesis: S.M. in Engineering and Management, Massachusetts Institute of Technology, System Design and Management Program, 2018.
Cataloged from PDF version of thesis.
Includes bibliographical references (pages 103-108).
The advent of commercial launch systems has brought about a new age of space launch vehicle design. In order to survive in a competitive market, space launch providers must design systems with new technologies in shorter development times. This changing nature of space launch vehicle design requires a new way to perform safety analysis. Traditional hazard analysis techniques do not deliver adequate insight early in the design process, when most of the safety-related decisions are made. Early design decisions are often made using "lessons-learned" from previous launch systems, rather than interactive feedback from the new vehicle design actually being developed. Furthermore, traditional techniques use reliability theory as their foundation, resulting in the use of excessive design margin and redundancy as the "default" vehicle design choices. This equivocation of safety and reliability may have made sense for simpler launch vehicles of the past, but most modern space launch vehicle accidents have resulted from incorrect software specifications, component interaction accidents, and other design errors independent of the reliability of individual components. The space launch industry needs safety analysis methods and design processes that identify and correct these hazards early in the vehicle design process, when modifications to correct safety issues are more effective and less costly. This work shows how Systems-Theoretic Process Analysis (STPA) can been used as a powerful tool to identify, mitigate, and possibly eliminate hazards throughout the entire space launch vehicle lifecycle. This work begins by reviewing traditional hazard analysis techniques and the changing nature of launch vehicle accidents. Next, it describes how STPA can be integrated into the space launch vehicle lifecycle to design safer systems. It then demonstrates the safety-guided design of a small-lift launch vehicle using STPA. Finally, this work shows how STPA can be used to satisfy regulatory and range safety requirements. The thesis of this work is that integration of STPA into the design of space launch vehicles can make a significant contribution to reducing launch vehicle accidents.
by John M. Rising.
S.M. in Engineering and Management
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Moss, Vaughan. "Thermal design and analysis of the SKA SA MeerKAT Digitiser." Master's thesis, University of Cape Town, 2018. http://hdl.handle.net/11427/29782.

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The Square Kilometre Array Project is a multi-national venture attempting to build the world's largest radio telescope. Australia and South Africa (together with other African countries), will be host to the SKA site. Both countries are building pre-cursor radio telescopes to demonstrate their ability to successfully host the project. Square Kilometre Array South Africa (SKA SA) is currently constructing the MeerKAT Radio Telescope in the Karoo Desert. Radio telescopes are conventionally designed to have the signal Digitiser located in the pedestal of the radio telescope antenna structure to shield the incoming radio signal from being contaminated by the electromagnetic interference (EMI)/radio frequency interference (RFI) noise created by the Digitiser electronics. However, if a Digitiser could be placed near the antenna feed, this would decrease the length of the signal path between the receiver and the Digitiser, which would decrease noise on the signal. The aim of this thesis is to present a viable thermal design for an externally, near-feed mounted, passively cooled Digitiser on the MeerKAT Radio Telescope. This has never been done before. Through calculation, simulation and design iteration this aim was achieved, resulting in an operational Digitiser system which is being used on the MeerKAT Radio Telescope and could potentially also be used in SKA Phase 1.
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Ball, Jeffrey Craig. "Design and analysis of multifunctional composite structures for nano-satellites." Thesis, Cape Peninsula University of Technology, 2017. http://hdl.handle.net/20.500.11838/2572.

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Thesis (MTech (Mechanical Engineering))--Cape Peninsula University of Technology, 2017.
The aim of this thesis is to investigate the applications of multifunctional compos- ite (MFC) technology to nano-satellite structures and to produce a working concept design, which can be implemented on future Cube-Satellites (CubeSats). MFC tech- nologies can be used to optimise the performance of the satellite structure in terms of mass, volume and the protection it provides. The optimisation of the structure will allow further room for other sub-systems to be expanded and greater payload allowance. An extensive literature view of existing applications of MFC materials has been conducted, along with the analysis of a MFC CubeSat structural design account- ing for the environmental conditions in space and well-known design practices used in the space industry. Numerical analysis data has been supported by empirical analysis that was done where possible on the concept material and structure. The ndings indicate that the MFC technology shows an improvement over the conventional alu- minium structures that are currently being used. Improvements in rigidity, mass and internal volume were observed. Additional functions that the MFC structure o ers include electrical circuitry and connections through the material itself, as well as an increase electromagnetic shielding capability through the use of carbon- bre composite materials. Empirical data collected on the MFC samples also show good support for the numerical analysis results. The main conclusion to be drawn from this work is that multifunctional composite materials can indeed be used for nano-satellite structures and in the same light, can be tailor-made to the speci c mission requirements of the satellite. The technology is in its infancy still and has vast room for improvement and technological development beyond this work and well into the future. Further improvements and additional functions can be added through the inclusion of various other materials.
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Brathwaite, Joy Danielle. "Value-informed space systems design and acquisition." Diss., Georgia Institute of Technology, 2011. http://hdl.handle.net/1853/43748.

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Investments in space systems are substantial, indivisible, and irreversible, characteristics that make them high-risk, especially when coupled with an uncertain demand environment. Traditional approaches to system design and acquisition, derived from a performance- or cost-centric mindset, incorporate little information about the spacecraft in relation to its environment and its value to its stakeholders. These traditional approaches, while appropriate in stable environments, are ill-suited for the current, distinctly uncertain and rapidly changing technical, and economic conditions; as such, they have to be revisited and adapted to the present context. This thesis proposes that in uncertain environments, decision-making with respect to space system design and acquisition should be value-based, or at a minimum value-informed. This research advances the value-centric paradigm by providing the theoretical basis, foundational frameworks, and supporting analytical tools for value assessment of priced and unpriced space systems. For priced systems, stochastic models of the market environment and financial models of stakeholder preferences are developed and integrated with a spacecraft-sizing tool to assess the system's net present value. The analytical framework is applied to a case study of a communications satellite, with market, financial, and technical data obtained from the satellite operator, Intelsat. The case study investigates the implications of the value-centric versus the cost-centric design and acquisition choices. Results identify the ways in which value-optimal spacecraft design choices are contingent on both technical and market conditions, and that larger spacecraft for example, which reap economies of scale benefits, as reflected by their decreasing cost-per-transponder, are not always the best (most valuable) choices. Market conditions and technical constraints for which convergence occurs between design choices under a cost-centric and a value-centric approach are identified and discussed. In addition, an innovative approach for characterizing value uncertainty through partial moments, a technique used in finance, is adapted to an engineering context and applied to priced space systems. Partial moments disaggregate uncertainty into upside potential and downside risk, and as such, they provide the decision-maker with additional insights for value-uncertainty management in design and acquisition. For unpriced space systems, this research first posits that their value derives from, and can be assessed through, the value of information they provide. To this effect, a Bayesian framework is created to assess system value in which the system is viewed as an information provider and the stakeholder an information recipient. Information has value to stakeholders as it changes their rational beliefs enabling them to yield higher expected pay-offs. Based on this marginal increase in expected pay-offs, a new metric, Value-of-Design (VoD), is introduced to quantify the unpriced system's value. The Bayesian framework is applied to the case of an Earth Science satellite that provides hurricane information to oil rig operators using nested Monte Carlo modeling and simulation. Probability models of stakeholders' beliefs, and economic models of pay-offs are developed and integrated with a spacecraft payload generation tool. The case study investigates the information value generated by each payload, with results pointing to clusters of payload instruments that yielded higher information value, and minimum information thresholds below which it is difficult to justify the acquisition of the system. In addition, an analytical decision tool, probabilistic Pareto fronts, is developed in the Cost-VoD trade space to provide the decision-maker with additional insights into the coupling of a system's probable value generation and its associated cost risk.
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Trisno, Sugianto. "Design and analysis of advanced free space optical communication systems." College Park, Md. : University of Maryland, 2006. http://hdl.handle.net/1903/3400.

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Thesis (Ph. D.) -- University of Maryland, College Park, 2006.
Thesis research directed by: Electrical Engineering. Title from t.p. of PDF. Includes bibliographical references. Published by UMI Dissertation Services, Ann Arbor, Mich. Also available in paper.
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Babilis, Lambros. "Micro-Formian for the analysis and design of space frames." Thesis, University of Surrey, 1988. http://epubs.surrey.ac.uk/842973/.

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The analysis and design of a triactive frame involves the generation of a large amount of information describing the structure, in the form of numerical data. The generation of the required data is time consuming and prone to error. The present work attempts to offer a convenient computer assisted method for automated data generation. Micro-Formian, the computer program written for this purpose, is based on the ideas of formex algebra, which have been expanded in order to make better use of the available technology. The main features of Micro-Formian are its user-friendliness, its portability and its power in the generation of data. The user friendliness is achieved by an on-screen manual and a continuous dialogue with the user. The data generation procedures are based on the principles of formex algebra and the concept of geometric potential. The portability is achieved by using ANSI standard Pascal and by expressing all the hardware dependent variables in a parametric form. The research is, in essence, an investigation, into the philosophy behind computer aided structural analysis, whereby it examines the practicality of an interactive computing system for the automatic handling of structural design. A new technique related to mesh generation is implemented in an attempt to investigate the degree of optimization that can be achieved through a semi-automated procedure.
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Nakanishi, Hideyuki. "Design and Analysis of Social Interaction in Virtual Meeting Space." 京都大学 (Kyoto University), 2001. http://hdl.handle.net/2433/150615.

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本文データは平成22年度国立国会図書館の学位論文(博士)のデジタル化実施により作成された画像ファイルを基にpdf変換したものである
Kyoto University (京都大学)
0048
新制・課程博士
博士(情報学)
甲第9064号
情博第35号
新制||情||8(附属図書館)
UT51-2001-F394
京都大学大学院情報学研究科社会情報学専攻
(主査)教授 石田 亨, 教授 林 春男, 教授 酒井 徹朗
学位規則第4条第1項該当
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Books on the topic "Design Space Analysis"

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R, Wertz James, and Larson Wiley J, eds. Space mission analysis and design. Dordrecht: Kluwer, 1991.

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Larson, Wiley J., and James R. Wertz, eds. Space Mission Analysis and Design. Dordrecht: Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2692-2.

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Wertz, James R., and Wiley J. Larson, eds. Space Mission Analysis and Design. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3794-2.

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J, Larson Wiley, and Wertz James Richard, eds. Space mission analysis and design. 2nd ed. Torrance, Calif: Microcosm, 1992.

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Flabel, Jean-Claude. Practical stress analysis for design engineers: Design and analysis of aerospace vehicle structures. Hayden Lake, Idaho: Lake City Pub. Co., 1997.

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White, Edward T. Space adjacency analysis: Diagramming information for architectural design. Tucson, Ariz. (P.O. Box 41083, Tucson 85717): Architectural Media, 1986.

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1950-, Eekhout Mick, and Suresh G. R, eds. Analysis, design and construction of steel space frames. London: Thomas Telford, 2002.

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Hammond, Walter E. Space transportation: A systems approach to analysis and design. Reston, VA: American Institute of Aeronautics and Astronautics, 1999.

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Motro, René. Structural morphology and configuration processing of space structures. Essex: Multi-Science Pub., 2009.

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Structural morphology and configuration processing of space structures. Essex: Multi-Science Pub., 2009.

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Book chapters on the topic "Design Space Analysis"

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Sackheim, Robert L., Robert S. Wolf, and Sidney Zafran. "Space Propulsion Systems." In Space Mission Analysis and Design, 579–606. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3794-2_17.

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Wertz, James R. "Space Mission Geometry." In Space Mission Analysis and Design, 79–112. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3794-2_5.

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Sackheim, Robert L., Robert S. Wolf, and Sidney Zafran. "Space Propulsion Systems." In Space Mission Analysis and Design, 637–64. Dordrecht: Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2692-2_17.

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Wertz, James R. "Space Mission Geometry." In Space Mission Analysis and Design, 93–127. Dordrecht: Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2692-2_5.

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Karuri, Kingshuk, and Rainer Leupers. "The ASIP Design Space." In Application Analysis Tools for ASIP Design, 11–34. New York, NY: Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-8255-1_2.

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Ely, Neal, Thomas P. O’Brien, and Herbert Hecht. "Space Logistics and Reliability." In Space Mission Analysis and Design, 633–56. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3794-2_19.

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Ely, Neal, Thomas P. O’Brien, and Herbert Hecht. "Space Logistics and Reliability." In Space Mission Analysis and Design, 693–714. Dordrecht: Springer Netherlands, 1992. http://dx.doi.org/10.1007/978-94-011-2692-2_19.

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Cheng, Daizhan, Xiaoming Hu, and Tielong Shen. "Topological Space." In Analysis and Design of Nonlinear Control Systems, 29–46. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-11550-9_2.

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Reeves, Emery. "Spacecraft Design and Sizing." In Space Mission Analysis and Design, 255–300. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3794-2_10.

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Wirin, William B., and Darren S. McKnight. "Limits on Mission Design." In Space Mission Analysis and Design, 683–710. Dordrecht: Springer Netherlands, 1991. http://dx.doi.org/10.1007/978-94-011-3794-2_21.

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Conference papers on the topic "Design Space Analysis"

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Tuncer, Bige, and Sevil Sariyildiz. "Design Analysis Network - An educational environment for architectural analysis." In eCAADe 2006: Communicating Space(s). eCAADe, 2006. http://dx.doi.org/10.52842/conf.ecaade.2006.206.

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Lin, Joy. "Model-Based Design and Model Analysis of Fault and Mode Designs." In AIAA SPACE 2009 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-6644.

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Nardi, Luigi, David Koeplinger, and Kunle Olukotun. "Practical Design Space Exploration." In 2019 IEEE 27th International Symposium on Modeling, Analysis, and Simulation of Computer and Telecommunication Systems (MASCOTS). IEEE, 2019. http://dx.doi.org/10.1109/mascots.2019.00045.

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Chen, Su, Hu Wang, Yaoke Xue, Meiying Liu, and Lingguang Wang. "Design and analysis of push-broom optical camera's following windows." In Space Optics and Earth Imaging and Space Navigation, edited by Carl Nardell, Suijian Xue, and Huaidong Yang. SPIE, 2017. http://dx.doi.org/10.1117/12.2284267.

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Shin, Choong-Soo, Kwon-Hee Lee, and Gyung-Jin Park. "Robust structural optimization using design axioms in a discrete design space." In 8th Symposium on Multidisciplinary Analysis and Optimization. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-4808.

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Gablonsky, Joerg. "Computing Architectures for Design Space Exploration Methods." In 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-5958.

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Richardson, Gregory, Jay Penn, and Paul Collopy. "Value-Centric Analysis and Value-Centric Design." In AIAA SPACE 2010 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-8861.

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Lee, Gene, Elizabeth Jordan, Robert Shishko, Olivier de Weck, Nii Armar, and Afreen Siddiqi. "Design of Experiments in Campaign Logistics Analysis." In AIAA SPACE 2008 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-7684.

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Zuniga, Allison, David McKissock, and Charles Bard. "Integrated Design Analysis for the Constellation Architecture." In AIAA SPACE 2007 Conference & Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-6138.

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Piscitelli, R., and A. D. Pimentel. "Design space pruning through hybrid analysis in system-level design space exploration." In 2012 Design, Automation & Test in Europe Conference & Exhibition (DATE 2012). IEEE, 2012. http://dx.doi.org/10.1109/date.2012.6176600.

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Reports on the topic "Design Space Analysis"

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Hartunian, R., B. Moss, M. Wolfe, J. Statsinger, and L. Forrest. Space Transportation Analysis and Design. Fort Belvoir, VA: Defense Technical Information Center, March 1992. http://dx.doi.org/10.21236/ada250629.

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Hartunian, R., B. Moss, M. G. Wolfe, J. Statsinger, and L. Forrest. Space Transportation Analysis and Design (Reissue A). Fort Belvoir, VA: Defense Technical Information Center, February 1993. http://dx.doi.org/10.21236/ada262752.

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Parashar, Neha. Design Space Analysis and a Novel Routing Agorithm for Unstructured Networks-on-Chip. Portland State University Library, January 2000. http://dx.doi.org/10.15760/etd.89.

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Schock, Alfred, Meera Mukunda, and G. Summers. Analysis, Optimization, and Assessment of Radioisotope Thermophotovoltaic System Design for an Illustrative Space Mission. Office of Scientific and Technical Information (OSTI), June 1994. http://dx.doi.org/10.2172/1034425.

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Schock, Alfred, Meera Mukunda, Chuen T. Or, Vasanth Kumar, and G. Summers. Design, Analysis, and Optimization of a Radioisotope Thermophotovoltaic (RTPV) Generator, and its Applicability to an Illustrative Space Mission. Office of Scientific and Technical Information (OSTI), October 1994. http://dx.doi.org/10.2172/1033365.

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Minson, Valrie, Laura I. Spears, Adrian Del Monte, Margaret Portillo, Jason Meneely, Sara Gonzalez, and Jean Bossart. Library Impact Research Report: Facilitating Innovative Research, Creative Thinking, and Problem Solving. Association of Research Libraries, September 2022. http://dx.doi.org/10.29242/report.uflorida2022.

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As part of ARL’s Research Library Impact Framework initiative, the Marston Science Library (MSL) of the University of Florida (UF) George A. Smathers Libraries partnered with the UF Department of Interior Design (IND) to explore how research libraries facilitate innovation, creativity, and problem-solving competencies among their patrons. The MSL-IND team explored a three-tiered hypothesis that included: (1) students’ use of library spaces can contribute to building knowledge and practical applications for library space renovations; (2) student perceptions of space desirability as measured by the Place-based Semantic Differential can be used to indicate gaps in the library space facilitation of creativity; and (3) the creative thought process requires spaces that are diverse, flexible, and under a certain amount of student control. The research team developed a mixed-method study that included a spatial analysis, a survey utilizing an adjective checklist, and several focus groups designed to validate the adjective checklist. The research team analysis of the resulting data identified recommendations related to creating a sense of place, solving for the group by addressing the individual, offering a palette of posture, increasing biophilia, and offering choice and control.
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Collins, Clarence O., and Tyler J. Hesser. altWIZ : A System for Satellite Radar Altimeter Evaluation of Modeled Wave Heights. Engineer Research and Development Center (U.S.), February 2021. http://dx.doi.org/10.21079/11681/39699.

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This Coastal and Hydraulics Engineering Technical Note (CHETN) describes the design and implementation of a wave model evaluation system, altWIZ, which uses wave height observations from operational satellite radar altimeters. The altWIZ system utilizes two recently released altimeter databases: Ribal and Young (2019) and European Space Agency Sea State Climate Change Initiative v.1.1 level 2 (Dodet et al. 2020). The system facilitates model evaluation against 1 Hz1 altimeter data or a product created by averaging altimeter data in space and time around model grid points. The system allows, for the first time, quantitative analysis of spatial model errors within the U.S. Army Corps of Engineers (USACE) Wave Information Study (WIS) 30+ year hindcast for coastal United States. The system is demonstrated on the WIS 2017 Atlantic hindcast, using a 1/2° basin scale grid and a 1/4° regional grid of the East Coast. Consistent spatial patterns of increased bias and root-mean-square-error are exposed. Seasonal strengthening and weakening of these spatial patterns are found, related to the seasonal variation of wave energy. Some model errors correspond to areas known for high currents, and thus wave-current interaction. In conjunction with the model comparison, additional functions for pairing altimeter measurements with buoy data and storm tracks have been built. Appendices give information on the code access (Appendix I), organization and files (Appendix II), example usage (Appendix III), and demonstrating options (Appendix IV).
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Panchenko, Liubov F., Tetiana A. Vakaliuk, and Kateryna V. Vlasenko. Augmented reality books: concepts, typology, tools. [б. в.], November 2020. http://dx.doi.org/10.31812/123456789/4414.

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The article discussed the usage of augmented reality books in educational process. The object of research is augmented reality books. The subject of the study is the concepts and classification of augmented reality books; digital story making tools that emphasize child-teacher co-operation; difficulties in augmented reality using. The methods of research are: the analysis of publications about the issue; the analysis of digital tools capabilities; systematization and generalization of research information. In the article the facet classification for augmented books is proposed; the main facets are: reality- virtuality continuum, type of augmented materials, device types, type of interaction, spatial space of book, book’s category. Content for a module of a specialty course about augmented reality books for the system of professional training and retraining for educators in postgraduate education is discussed. Some samples of tasks for educators are presented: audio augmented book about world’s books monuments; analysis augmented reality examples in the textbook of the New Ukrainian school (subject name, topic, didactic tasks, quality of implementation, directions of expansion etc.), search and analysis augmented books according to the professional interests of the educators; discussion how augmented reality can help to improve student motivation with accent to attention, relevance, confidence and satisfaction; group work about design and creation a fragment of own textbook with augmented reality.
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Dudley, J. P., and S. V. Samsonov. SAR interferometry with the RADARSAT Constellation Mission. Natural Resources Canada/CMSS/Information Management, 2022. http://dx.doi.org/10.4095/329396.

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The RADARSAT Constellation Mission (RCM) is Canada's latest system of C-band Synthetic Aperture Radar (SAR) Earth observation satellites. The system of three satellites, spaced equally in a common orbit, allows for a rapid four-day repeat interval. The RCM has been designed with a selection of stripmap, spotlight, and ScanSAR beam modes which offer varied combinations of spatial resolution and coverage. Using Differential Interferometric Synthetic Aperture Radar (DInSAR) techniques, the growing archive of SAR data gathered by RCM can be used for change detection and ground deformation monitoring for diverse applications in Canada and around the world. In partnership with the Canadian Space Agency (CSA), the Canada Centre for Mapping and Earth Observation (CCMEO) has developed an automated system for generating standard and advanced deformation products and change detection from SAR data acquired by RCM and RADARSAT-2 satellites using DInSAR processing methodology. Using this system, this paper investigates four key interferometric properties of the RCM system which were not available on the RADARSAT-1 or RADARSAT-2 missions: The impact of the high temporal resolution of the four-day repeat cycle of the RCM on temporal decorrelation trends is tested and fitted against simple temporal decay models. The effect of the normalization and the precision of the radiometric calibration on interferometric spatial coherence is investigated. The performance of the RCM ScanSAR mode for wide area interferometric analysis is tested. The performance of the novel RCM Compact-polarization (CP) mode for interferometric analysis is also investigated.
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Шестопалова (Бондар), Катерина Миколаївна, and Олена Петрівна Шестопалова. Support of Inclusive Education in Kryvyi Rig. Padua, Italy, 2019. http://dx.doi.org/10.31812/123456789/3234.

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An analysis of the system of training, the implementation of a pilot project "SUPPORT OF INCLUSIVE EDUCATION IN KRYVYI RIG". The team that worked in project by GIZ (Deutsche Gesellschaft für Internationale Zusammenarbeit (GIZ) GmbH) create strategy for training teachers that include 6 modules: 1) regulatory and legislative framework for inclusive education; 2) inclusion ethics and philosophy; universal design and reasonable accommodation of educational space; 3) support team: interdisciplinary interation; algorithm of provision of psycho-pedagogical, corrective and development services; 4) individualization of the educational process; 5) competences of the teacher in inclusive education: strategies of teaching in inclusive education, method of collaborative learning, integration of technology into the discipline teaching methods, peculiarities of formation of mathematical concepts in children with special needs, difficulties with reading mastering and correction of dyslexia in children with special educational needs, correction and development of sense side of reading, development of intelligence of a child with SEN with the help of kinesiology methods, cooperation of teacher, psychologist and parents of a child with special educational needs, five levels can be associated with parents engagement; 6) work with children with behavior problems; resource room as the method of a child specific sensor needs satisfaction.
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