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Model Based Aircraft Control System Design And Simulation
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.ORCID iD: 0000-0002-1301-7931
Linköping University, Department of Management and Engineering, Machine Design. Linköping University, The Institute of Technology.
Linköping University, Department of Management and Engineering, Fluid and Mechatronic Systems. Linköping University, The Institute of Technology.
2010 (English)In: 27th Congress of the International Council of the Aeronautical Sciences 2010 (ICAS 2010), Proceedings of a meeting held 19-24 September 2010, Nice, France. / [ed] Professor I Grant, Optimage Ltd. on behalf of the International Council of the Aeronautical Sciences (ICAS) , 2010, 3338-3347 p.Conference paper, Published paper (Refereed)
Abstract [en]

Development of modern aircrafts has become more and more expensive and time consuming. In order to minimize the development cost, an improvement of the conceptual design phase is needed. The desired goal of the project is to enhance the functionality of an in house produced framework conducted at theDepartment of Machine Design, Link¨ping University, consisting of parametric aircraft models used for conceptual design. The former part of the work consists of the construction of geometric aircraft control surfaces such as flaps, aileron, rudder and elevator parametrically in CATIA V5. The next part of the work involves designing and simulating an Inverse dynamic model in Dymola software. An Excel interface has been developed between CATIA and Dymola. Parameters can be varied in the interface as per user specification; these values are sent to CATIA or Dymola and vice versa. The constructed concept model of control surfaces has been tested for different aircraft shapes and layout. An interface is developed between CATIA, Dymola and Tornado. An optimization case is performed to visualize the automation capability of choosing an actuator from a database for the proposed framework, and enhance the early design phases for aircraft conceptual design.

Place, publisher, year, edition, pages
Optimage Ltd. on behalf of the International Council of the Aeronautical Sciences (ICAS) , 2010. 3338-3347 p.
Keyword [en]
Aircraft Conceptual Design, Knowledge Based Design, Control System Design, Design Optimization
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:liu:diva-70558Local ID: 978-1-61782-049-6ISBN: 978-0-9565333-0-2 (print)OAI: oai:DiVA.org:liu-70558DiVA: diva2:440443
Conference
ICAS 2010, 27th Congress of International Council of the Aeronautical Sciences, 19-24 September, Nice Frankrike
Available from: 2011-09-12 Created: 2011-09-12 Last updated: 2015-06-02Bibliographically approved
In thesis
1. Knowledge Based Integrated Multidisciplinary Aircraft Conceptual Design
Open this publication in new window or tab >>Knowledge Based Integrated Multidisciplinary Aircraft Conceptual Design
2014 (English)Licentiate thesis, comprehensive summary (Other academic)
Abstract [en]

With the ever growing complexity of aircrafts, new tools and eventually methods to use these tools are needed in aircraft conceptual design. To reduce the development cost, an enhancement in the conceptual design is needed.

This thesis presents a knowledge-based aircraft geometry design tool RAPID and the methodology applied in realizing the design. The parameters used to create a geometry need to be exchange between different tools. This is achieved by using a centralized database or onedata concept. One-database will enable creating a less number of cross connections between different tools to exchange data with one another. Different types of aircraft configurations can be obtained with less effort. As RAPID is developed based on relational design, any changes made to the geometric model will update automatically. The geometry model is carefully defined to carry over to the preliminary design.

The validation of RAPID is done by implementing it in different aircraft design courses at Linköping University. In the aircraft project course, RAPID was effectively used and new features were added to the obtained desired design. Knowledge-base is used to realize the design performance for the geometry with an integrated database approach for a multidisciplinary aircraft conceptual design.

Place, publisher, year, edition, pages
Linköping: Linköping University Electronic Press, 2014. 52 p.
Series
Linköping Studies in Science and Technology. Thesis, ISSN 0280-7971 ; 1661
Keyword
Knowledge-base, Aircraft, Conceptual Design, CAD, XML Database, Multidisciplinary, Optimization
National Category
Engineering and Technology
Identifiers
urn:nbn:se:liu:diva-106925 (URN)10.3384/lic.diva-106925 (DOI)978-91-7519-328-1 (ISBN)
Presentation
2014-06-16, ACAS, A-building, Campus Valla, Linköpings universitet, Linköping, 10:15 (English)
Opponent
Supervisors
Available from: 2014-05-27 Created: 2014-05-27 Last updated: 2015-06-02Bibliographically approved

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Venkata, Raghu. C. M.Tarkian, MehdiJouannet, Christopher

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