Academic literature on the topic 'Parameterized design'

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Journal articles on the topic "Parameterized design"

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YAO, Huixue. "Parameterized Database Design of Vehicle Brakes." Chinese Journal of Mechanical Engineering 44, no. 10 (2008): 255. http://dx.doi.org/10.3901/jme.2008.10.255.

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Wang, Yan Zhen, Jian Ping Wang, Sun Sun, and Yan Mei Li. "Women's Suit Pattern Parameterized Intelligent Design." Advanced Materials Research 331 (September 2011): 578–81. http://dx.doi.org/10.4028/www.scientific.net/amr.331.578.

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To study the parameterized intelligent generation of women’s suit pattern, it is proposed a concept about rapid generation of individualize pattern. Focused on research principal parts (Body modular, Sleeve modular and lapel modular) of lady’s suit automatic generation system and built up the curve mathematics parameters model, it obtained the data base of system structure. Realization of suit showed how to establish the parametric model of body, sleeve and collar. It began to set up a automatic system about interactive pattern tentatively on the base of VC++ and Arcobjects.
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Wang, Lijing. "A Parameterized Mannequin for Apparel Design." Journal of Fiber Bioengineering and Informatics 1, no. 2 (June 2008): 117–24. http://dx.doi.org/10.3993/jfbi09200805.

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Consel, Charles, and Siau Cheng Khoo. "Parameterized partial evaluation." ACM SIGPLAN Notices 26, no. 6 (June 1991): 92–106. http://dx.doi.org/10.1145/113446.113454.

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Zhou, Si Zhu, and Si Zhang. "Parametric Design of the Coupling of Oilfield Turbodrill." Key Engineering Materials 579-580 (September 2013): 305–9. http://dx.doi.org/10.4028/www.scientific.net/kem.579-580.305.

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Through discussing the working characteristics of turbodrill and structural particularity of the coupling, the feasibility of couplings series design by parameterized design method has been presented. Through taking advantage of Proe, selecting a turbodrill with diameter of 195mm as the original model, the series design and parameterized design of coupling have been achieved. This paper puts forward four design skills through analyzing the parameterized design of the coupling. The method has been developed and used in the series design of oilfield turbodrill in Yangtze university of China.
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Séquin, C. H., and E. K. Smyrl. "Parameterized Ray-tracing." ACM SIGGRAPH Computer Graphics 23, no. 3 (July 1989): 307–14. http://dx.doi.org/10.1145/74334.74365.

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Cheng, Yongxi, Ding-Zhu Du, Ker-I. Ko, and Guohui Lin. "On the Parameterized Complexity of Pooling Design." Journal of Computational Biology 16, no. 11 (November 2009): 1529–37. http://dx.doi.org/10.1089/cmb.2008.0224.

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Zhao, H. Z., and F. L. Yin. "Research of Missile Parameterized Design System with ProToolkit." Advanced Materials Research 215 (March 2011): 393–96. http://dx.doi.org/10.4028/www.scientific.net/amr.215.393.

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The system structure of missile parameterized design is put forward to solve the repeat problems in the process of designing and manufacturing missiles. It is illustrated that in Pro/E environment the combination of missile design parameters with constraint relation is adopted to develop missile parameterized system with VC++6.0 and Pro/Toolkit used as secondary development tools for the secondary development and through the dynamic linkage, and the missile parameterized design system is integrated with Pro/E tightly. The missiles designers can obtain series of projectiles or new types of projectiles by modifying main design parameters, which making it possible to meet with a certain standard tactically and technically and shorten the cycle of designing new products.
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Hou, Shou Ming, Yong Xian Liu, Bo Yan, and Zhong Qi Sheng. "Research on Parameterized Modeling Method of Parts and Components Library for Rapid Response System." Applied Mechanics and Materials 16-19 (October 2009): 368–73. http://dx.doi.org/10.4028/www.scientific.net/amm.16-19.368.

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In order to meet the requirement of mass customization and rapid response design, a hierarchical parameterized modeling method of parts and components library is proposed. The library of parts and components is building up with NX/Open development tools based on the three-dimensional design software platform. According to this method, the master model technique is integrated with top-down modeling method to facilitate the parameterized modeling and variant design of product family. The parameterized modeling process is also demonstrated in details in this paper. As an example, a tools management system for NC machine tools rapid design is developed. It shows hierarchical parameterized modeling method is a practical and effective method of constructing the product resources library.
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Shaker, George S. A., Mohamed H. Bakr, Nagula Sangary, and Safieddin Safavi-Naeini. "ACCELERATED ANTENNA DESIGN METHODOLOGY EXPLOITING PARAMETERIZED CAUCHY MODELS." Progress In Electromagnetics Research B 18 (2009): 279–309. http://dx.doi.org/10.2528/pierb09091109.

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Dissertations / Theses on the topic "Parameterized design"

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Weicker, Phillip J. "A parameterized, sensitivity-driven EM design environment /." Thesis, McGill University, 2005. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=82643.

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This thesis deals with the application of sensitivity analysis to a variational geometry environment for the optimization of the design of electromagnetic devices. Through a graphical user interface, an electromagnetic device is sketched in a free-hand manner. The device topology is stored in a parameteric fashion. The sketch provides the topology (geometric entities and their interconnection) and defines the device, where changing the parameters provides all the possible devices under consideration. The performance of the device is computed using a commerical finite-element package. The effect of changing the system parameters on the device performance is investigated and used to modify the device to change the performance in the desired way. Significant gains in optimization performance are realized through the use of deterministic optimization techniques.
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Sridhar, Nigamanth. "Dynamically reconfigurable parameterized components." Columbus, Ohio : Ohio State University, 2004. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu1078930623.

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Thesis (Ph. D.)--Ohio State University, 2004.
Title from first page of PDF file. Document formatted into pages; contains xv, 147 p.; also includes graphics. Includes abstract and vita. Advisors: Paolo A.G. Sivilotti and Bruce W. Weide, Dept. of Computer and Information Science. Includes bibliographical references (p. 140-147).
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Singh, Aakash Narender, and Vijay Govindharajan. "Automated generic parameterized design of aircraft fairing and windshield." Thesis, Linköpings universitet, Fluida och mekatroniska system, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-75858.

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The process of design is time consuming and result oriented. There is always a better scope for any design that reduces the time with better precision. Considering this as a major factor during design process, two of the vital parts of the aircraft conceptual design are taken into account where a lot of time can be saved. Major components considered in this work are fairings for the lift generating surfaces and cockpit windshield. In this work the major inference is to reduce the time spent on the initial conceptual design. The two components designed in this work are fairings and windshield. The fairing design in this work provides a flexible template which can be used for various fuselage and wing configurations for transport aircrafts. The windshield is classified into two types in this work, flat and blend windshield. Both the type of windshields can be implemented on appropriate fuselage. Both the components are designed to be implemented in single pilot as well as double pilot aircrafts. They also have parameters which can be modified according to the user requirement. The changes in the parameters provide the change in shape, size and volume of the components. The software used for this is CATIA V5. The process is carried out using two automation methods available in CATIA namely Power-Copy and Knowledge pattern. A comparison between the effectiveness of two automation methods used in this work is performed.
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Uebelhart, Scott Alan 1975. "Non-deterministic design and analysis of parameterized optical structures during conceptual design." Thesis, Massachusetts Institute of Technology, 2006. http://hdl.handle.net/1721.1/39598.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2006.
Includes bibliographical references (p. 261-272).
The next generation of space observatories will use larger mirrors while meeting tighter optical performance requirements than current space telescopes. The spacecraft designs must satisfy the drive for low-mass, low-cost systems, and be robust to uncertainty since design validation will be based on analysis instead of pre-launch tests. Analytical techniques will be required to identify which technologies or structural architectures are most appropriate to meet conflicting system requirements, but traditionally, model-based dynamic analysis would only take place after a single point design is chosen. The challenges facing future space telescopes require a new approach to conceptual design, and motivate the creation of design tools to identify superior, robust designs earlier in the design lifecycle using model-based analysis methods. A conceptual design methodology is proposed, in which both nominal performance as well as robustness to uncertainty are evaluated across multiple design realizations. A modeling environment is created so that for any set of design variables, such as mirror architecture or dimensions of the spacecraft, a finite element model is automatically generate and analyzed.
(cont.) A frequency-based dynamic analysis is performed for each design realization using integrated disturbance-to-performance models that include control systems and vibration isolators. Next, the uncertainty in early stages of design is considered and Design of Experiments tools such as the analysis of variance are used to identify critical uncertainty parameters. Lastly, parametric uncertainties are propagated through the model to bound the outputs. Aspects of this methodology are applied to several telescopes in order to demonstrate the practicality of this approach in real-life design studies. Critical uncertainty parameter identification and uncertainty analysis tools are applied to the Terrestrial Planet Finder interferometer. A parameterized model is prepared and a trade-space analysis performed for the ground-based Thirty Meter Telescope. Finally, the methodology as a whole is applied to a new space telescope design employing lightweight mirrors and a segmented aperture. An exploration of the design space is followed by uncertainty evaluation of the optimal designs. Over 1200 unique design realizations are evaluated, and the architecture families that provide the best performance and robustness to uncertainty are identified.
by Scott Alan Uebelhart.
Ph.D.
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Endicott, Giles E. "Achieving speedup of design optimization by predicting parameterized aerodynamic simulations." Thesis, University of Southampton, 2009. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.536363.

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DIAZ, RUBEN GOMEZ. "A SYSTEM FOR GENERATION OF PARAMETERIZED MODELS FOR VESSELS DESIGN." PONTIFÍCIA UNIVERSIDADE CATÓLICA DO RIO DE JANEIRO, 2009. http://www.maxwell.vrac.puc-rio.br/Busca_etds.php?strSecao=resultado&nrSeq=14888@1.

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CONSELHO NACIONAL DE DESENVOLVIMENTO CIENTÍFICO E TECNOLÓGICO
Este trabalho situa-se numa das linhas de pesquisa da PUC-Rio de projeto de unidades flutuantes tais como, navios e plataformas semi-submersíveis. Nesta linha de pesquisa estão sendo desenvolvidos os programas gráficos MG (Mesh Generator) e o Sstab. O primeiro programa é um modelador geométrico por meio de seções transversais e gerador de malhas para modelos de estruturas flutuantes. O segundo programa é utilizado para a análise de estabilidade estática dos modelos gerados pelo MG. Este trabalho propõe um ambiente integrado de modelagem e de análise estática e dinâmica de estruturas flutuantes. O principal diferencial deste ambiente está no fato de possibilitar a geração automática de variantes de um determinado modelo padrão, a fim de atingir uma configuração desejada, seja no aspecto geométrico ou com relação a sua estabilidade estática. Este ambiente faz uso da linguagem Lua e é possível definir variáveis globais para serem utilizadas como parâmetros de modelagem que extraem, ou modificam, dados como comprimento, largura, altura etc. É possível parametrizar um modelo qualquer, em função de variáveis escolhidas pelo usuário, o que possibilita uma modelagem automática, com a variação de alguns destes parâmetros. Foram ainda desenvolvidas algumas ferramentas auxiliares que facilitam a modelagem de uma estrutura flutuante. Estas ferramentas verificam a consistência topológica de uma malha, gerar uma subdivisão gradativa das curvas cortadas e simplificar as novas malhas geradas. É possível também detectar se o modelo possui simetria num determinado plano e realizar, de forma automática, cortes do modelo final para diferentes calados.
This work is related to the PUC-Rio research area of vessel´s designs such as ships and semi-sub platforms. In this research area two softwares have been developed: MG and Sstab. The first is a geometric modeler based on cross sections and also on a mesh generator; the second is a software for the analysis of static and dynamic stability of MG models. This work proposes an integrated environment for modeling, and static and dynamic analysis of vessels. The main advantage of the proposed environment is that it is possible to obtain automatically variants of a specific model in order to achieve a desired configuration, not only in relation to geometry but also concerning the static stability aspect. This environment uses the Lua programming language and it is possible to define global variables to be used as parameters which retrieve or modify modeling values such as length, width, height, and so on. Any model can be parameterized, as a function of user chosen variables, which allows an automatic modeling with the variation of those parameters. There has been also developed some auxiliary tools which help the modeling of floating structures. Those tools verify the topological consistency of a mesh, generate a gradual subdivision of intersected curves and simplify the new generated meshes. They are also able to detect if the model has symmetry in relation to a certain plane, and sections can be automatically obtained according to different draughts.
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Malak, Richard J. Jr. "Using parameterized efficient sets to model alternatives for systems design decisions." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2008. http://hdl.handle.net/1853/26697.

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Thesis (Ph.D)--Mechanical Engineering, Georgia Institute of Technology, 2009.
Committee Chair: Paredis, Christiaan J.J.; Committee Member: Bras, Bert; Committee Member: Choudhary, Ruchi; Committee Member: McGinnis, Leon; Committee Member: Rosen, David. Part of the SMARTech Electronic Thesis and Dissertation Collection.
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Dai, Lei. "An Open Platform of Parameterized Shape Optimization based-on CAD/CAE Integration Technique." Reims, 2006. http://theses.univ-reims.fr/exl-doc/GED00000752.pdf.

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The main content in the research is developing an open platform of parameterized shape optimization based-on CAD/CAE integration technique. Through integration, structural analysis and design optimization are seamless combined with parametric geometry modeling and embed into the CAD system. POSHAPE can provide parameterized shape optimization method for 3D solid structure, spatial shell structure and cell structure of composite material. To realize such a general method, integration is the most essential part. In this platform, integration is realized includes: 1) Integrating structure analysis tool of different disciplinary with structure shape optimization. Structure response from different disciplinary will be studied according structure shape. 2) Integrating finite element modeling with parametric geometry modeling through Boundary Representative Tree (simplified as: B-Rep) used in solid modeling. Finite element model is parameterized to be dynamic regenerated during optimization design steps. 3) Parametric solid modeling is extended to realize parameterized surface modeling under integration between surface model definition and solid model. Parameterized finite element modeling of shell structure is also achieved which is similar to that of solid structure
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Sohaib, Muhammad. "Parameterized Automated Generic Model for Aircraft Wing Structural Design and Mesh Generation for Finite Element Analysis." Thesis, Linköpings universitet, Maskinkonstruktion, 2011. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-71264.

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This master thesis work presents the development of a parameterized automated generic model for the structural design of an aircraft wing. Furthermore, in order to perform finite element analysis on the aircraft wing geometry, the process of finite element mesh generation is automated. Aircraft conceptual design is inherently a multi-disciplinary design process which involves a large number of disciplines and expertise. In this thesis work, it is investigated how high-end CAD software‟s can be used in the early stages of an aircraft design process, especially for the design of an aircraft wing and its structural entities wing spars and wing ribs. The generic model that is developed in this regard is able to automate the process of creation and modification of the aircraft wing geometry based on a series of parameters which define the geometrical characteristics of wing panels, wing spars and wing ribs.Two different approaches are used for the creation of the generic model of an aircraft wing which are “Knowledge Pattern” and “PowerCopy with Visual Basic Scripting” using the CATIA V5 software. A performance comparison of the generic wing model based on these two approaches is also performed. In the early stages of the aircraft design process, an estimate of the structural characteristic of the aircraft wing is desirable for which a surface structural analysis (using 2D mesh elements) is more suitable. In this regard, the process of finite element mesh generation for the generic wing model is automated. The finite element mesh is generated for the wing panels, wing spars and wing ribs. Furthermore, the finite element mesh is updated based on any changes in geometry and the shape of the wing panels, wing spars or wing ribs, and ensure that all the mesh elements are always properly connected at the nodes. The automated FE mesh generated can be used for performing the structural analysis on an aircraft wing.
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Luo, Ping. "Design and Implementation of High Performance Algorithms for the (n,k)-Universal Set Problem." [College Station, Tex. : Texas A&M University, 2009. http://hdl.handle.net/1969.1/ETD-TAMU-2009-08-7033.

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Books on the topic "Parameterized design"

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IWPEC 2009 (2009 Copenhagen, Denmark). Parameterized and exact computation: 4th international workshop, IWPEC 2009, Copenhagen, Denmark, September 10-11, 2009 : revised selected papers. Berlin: Springer, 2009.

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Garris, Berle Jr. Analysis and design of a parameterized protocol convertor. 1985.

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Kandybowicz, Jason. Anti-contiguity. Oxford University Press, 2020. http://dx.doi.org/10.1093/oso/9780197509739.001.0001.

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This book develops a theory of wh- prosody according to which wh- expressions must avoid forming prosodic constituents with overt complementizers at the level of Intonational Phrase. The theory is inspired by Richards’s (2010, 2016) Contiguity Theory and is based empirically on asymmetries in the distribution of wh- items in five West African languages: Krachi (Kwa: Ghana), Bono (Kwa: Ghana), Wasa (Kwa: Ghana), Asante Twi (Kwa: Ghana), and Nupe (Benue-Congo: Nigeria). The observations and analyses stem from original fieldwork on all five languages and represent some of the first prosodic descriptions of the languages. The theory is shown to successfully derive a number of famous and less well-known asymmetries in wh- in-situ distribution in a variety of languages unrelated to those the theory was originally designed to analyze. Against the backdrop of data from eighteen languages, the theory is parameterized to account for wh- item distribution across typologically diverse languages.
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Book chapters on the topic "Parameterized design"

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Samer, Marko, and Helmut Veith. "Parameterized Vacuity." In Formal Methods in Computer-Aided Design, 322–36. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-30494-4_23.

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Thilikos, Dimitrios M. "Graph Minors and Parameterized Algorithm Design." In The Multivariate Algorithmic Revolution and Beyond, 228–56. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-30891-8_13.

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Ascia, Giuseppe, Vincenzo Catania, and Maurizio Palesi. "Tuning Methodologies for Parameterized Systems Design." In The Kluwer International Series in Engineering and Computer Science, 71–82. Boston, MA: Springer US, 2003. http://dx.doi.org/10.1007/978-1-4615-0351-4_8.

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Ruiz, José Luis, Yago Torroja, and José Luis García. "Design of a VME parameterized library for FPGAs." In Lecture Notes in Computer Science, 394–99. Berlin, Heidelberg: Springer Berlin Heidelberg, 1996. http://dx.doi.org/10.1007/3-540-61730-2_45.

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Yuan, Yabo, Bo Wang, and Bin Wu. "Parameterized Unified Modulation Model Design for Satellite Communications." In Proceedings of the 28th Conference of Spacecraft TT&C Technology in China, 501–12. Singapore: Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-4837-1_40.

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Bellegarde, Françoise, Célina Charlet, and Olga Kouchnarenko. "How to Compute the Refinement Relation for Parameterized Systems." In Formal Methods and Models for System Design, 181–209. Boston, MA: Springer US, 2004. http://dx.doi.org/10.1007/978-1-4020-8052-4_8.

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Chou, Ching-Tsun, Phanindra K. Mannava, and Seungjoon Park. "A Simple Method for Parameterized Verification of Cache Coherence Protocols." In Formal Methods in Computer-Aided Design, 382–98. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-30494-4_27.

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Bang-Jensen, Jørgen, Manu Basavaraju, Kristine Vitting Klinkby, Pranabendu Misra, M. S. Ramanujan, Saket Saurabh, and Meirav Zehavi. "Parameterized Algorithms for Survivable Network Design with Uniform Demands." In Proceedings of the Twenty-Ninth Annual ACM-SIAM Symposium on Discrete Algorithms, 2838–50. Philadelphia, PA: Society for Industrial and Applied Mathematics, 2018. http://dx.doi.org/10.1137/1.9781611975031.180.

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Kraft, Bodo, and Manfred Nagl. "Parameterized Specification of Conceptual Design Tools in Civil Engineering." In Applications of Graph Transformations with Industrial Relevance, 90–105. Berlin, Heidelberg: Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-25959-6_7.

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Hands, Padmini Srinivasan, Anand Srinivasan, and Gerard M. Vignes. "Database design with behavior and views using parameterized Petri nets." In OOER '95: Object-Oriented and Entity-Relationship Modeling, 158–69. Berlin, Heidelberg: Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/bfb0020529.

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Conference papers on the topic "Parameterized design"

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Givargis, Tony D., and Frank Vahid. "Parameterized system design." In the eighth international workshop. New York, New York, USA: ACM Press, 2000. http://dx.doi.org/10.1145/334012.334031.

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Koshel, R. John. "Optimization of Parameterized Lightpipes." In International Optical Design Conference. Washington, D.C.: OSA, 2006. http://dx.doi.org/10.1364/iodc.2006.tub1.

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Sanchez, Miguel Angel, Pedro Echeverria, Francisco Mansilla, and Marisa Lopez-Vallejo. "Designing highly parameterized hardware using xHDL." In Design Languages (FDL). IEEE, 2008. http://dx.doi.org/10.1109/fdl.2008.4641425.

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Jinjun Xiong, V. Zolotov, N. Venkateswaran, and C. Visweswariah. "Criticality computation in parameterized statistical timing." In 2006 Design Automation Conference. IEEE, 2006. http://dx.doi.org/10.1109/dac.2006.229166.

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Chaurasiya, Rohit, John Gustafson, Rahul Shrestha, Jonathan Neudorfer, Sangeeth Nambiar, Kaustav Niyogi, Farhad Merchant, and Rainer Leupers. "Parameterized Posit Arithmetic Hardware Generator." In 2018 IEEE 36th International Conference on Computer Design (ICCD). IEEE, 2018. http://dx.doi.org/10.1109/iccd.2018.00057.

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Shah, Shivani, Sahithi Meenakshi Vutakuru, and Nanditha P. Rao. "FPGA Accelerated Parameterized Cache Simulator." In 2021 22nd International Symposium on Quality Electronic Design (ISQED). IEEE, 2021. http://dx.doi.org/10.1109/isqed51717.2021.9424272.

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Gui, Yan, Dilin Pan, and Lixiang Zhang. "Parameterized Design of Centrifugal Fan's Impeller." In 2010 International Conference on Measuring Technology and Mechatronics Automation (ICMTMA 2010). IEEE, 2010. http://dx.doi.org/10.1109/icmtma.2010.554.

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Liu, Hongzheng, Lei Chen, Xiuzi Ye, Xiang Pan, and Qiuer Xu. "Parameterized Freeform Shape Design and Deformation." In 2007 International Conference on Multimedia and Ubiquitous Engineering (MUE'07). IEEE, 2007. http://dx.doi.org/10.1109/mue.2007.169.

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Zhu, Zhenhai. "A parameterized mask model for lithography simulation." In the 46th Annual Design Automation Conference. New York, New York, USA: ACM Press, 2009. http://dx.doi.org/10.1145/1629911.1630158.

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Murugappa, Purushotham, Amer Baghdadi, and Michel Jezequel. "Parameterized Area-efficient Multi-standard Turbo Decoder." In Design Automation and Test in Europe. New Jersey: IEEE Conference Publications, 2013. http://dx.doi.org/10.7873/date.2013.036.

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Reports on the topic "Parameterized design"

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Apostolatos, A., R. Rossi, and C. Soriano. D7.2 Finalization of "deterministic" verification and validation tests. Scipedia, 2021. http://dx.doi.org/10.23967/exaqute.2021.2.006.

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This deliverable focus on the verification and validation of the solvers of Kratos Multiphysics which are used within ExaQUte. These solvers comprise standard body-fitted approaches and novel embedded approaches for the Computational Fluid Dynamics (CFD) simulations carried out within ExaQUte. Firstly, the standard body-fitted CFD solver is validated on a benchmark problem of high rise building - CAARC benchmark and subsequently the novel embedded CFD solver is verified against the solution of the body-fitted solver. Especially for the novel embedded approach, a workflow is presented on which the exact parameterized Computer-Aided Design (CAD) model is used in an efficient manner for the underlying CFD simulations. It includes: A note on the space-time methods Verification results for the body-fitted solver based on the CAARC benchmark Workflow consisting of importing an exact CAD model, tessellating it and performing embedded CFD on it Verification results for the embedded solver based on a high-rise building API definition and usage
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