Optimal Wing Design

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2011 4th IEEE International Conference on Computer Science and Information Technology (ICCSIT 2011)

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The conference is an international forum for the presentation of technological advances and research results in the fields of Computer Science and Information Technology. The conference will bring together leading researchers, engineers and scientists in the domain of interest from around the world.


2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics (CAR 2010)

The purpose of the 2010 2nd International Asia Conference on Informatics in Control, Automation and Robotics (CAR 2010) is to bring together researchers, engineers and practitioners interested in the application of informatics to Control, Automation and Robotics.


2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics (ISSCAA)

Spacecraft Technologies, Aeronautics Technologies, Guidance and Navigation, Space Robots, Control Systems, Signal and Image Processing, Computational Intelligence, Emerging Technologies, Special Sessions


2010 International Conference on Educational and Network Technology (ICENT 2010)

The aim objective of ICENT 2010 is to provide a platform for researchers, engineers, academicians as well as industrial professionals from all over the world to present their research results and development activities in Educational and Network Technology.


Xplore Articles related to Optimal Wing Design

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  • Flight control system design for the flying-wing aircraft by using intelligent optimal seeking method

    Chai Xue; Wang Ganglin; Wu Zhe Informatics in Control, Automation and Robotics (CAR), 2010 2nd International Asia Conference on, 2010

    Most flying-wing aircrafts are static and dynamic unstable due to the lack of conventional stabilizers to control the plane in the longitudinal and the lateral directions, and the lateral-directional motion of the static instability flying-wing will cause the coupled longitudinal motion, so the control system is more complicated to design. With this motivation, the longitudinal and lateral-directional coupled motion of ...

  • Optimal design of aircraft wing structures: a computer aided design method

    Ampofo, J.; Ferguson, F. Automation Congress, 2002 Proceedings of the 5th Biannual World, 2002

    Aircraft weight plays a significant role in its design because of its dominating effects on the vehicle overall performance. Statistical results suggested that the amplification impact factor of any weight-carrying component is about 4.525. That is, a 1.0 lb reduction in the structural weight translates to 4.525 lb reduction in gross aircraft takeoff weight. This paper focuses on the preliminary ...

  • Design of an electron gun using computer optimization

    Lewis, B.M.; Tran, H.T.; Read, Michael E.; Ives, R.L. Plasma Science, IEEE Transactions on, 2004

    This paper considers an optimization technique in which the objective is attained via alterations to the physical geometry of the system. This optimization framework, to be considered in the context of electron guns, is known as optimal shape design. Optimal shape design has been used in a number of applications including wing design, magnetic tape design, and nozzle design, among ...

  • Development of a Flying Robot With a Pantograph-Based Variable Wing Mechanism

    Hara, N.; Tanaka, K.; Ohtake, H.; Wang, H.O. Robotics, IEEE Transactions on, 2009

    We develop a flying robot with a new pantograph-based variable wing mechanism for horizontal-axis rotorcrafts (cyclogyro rotorcrafts). A key feature of the new mechanism is to have a unique trajectory of variable wings that not only change angles of attack but also expand and contract according to wing positions. As a first step, this paper focuses on demonstrating the possibility ...

  • Design Gust Alleviation Controller for Highly Flexible Solar UAV

    Wang Rui; Zhu Xiaoping; Zhou Zhou Measuring Technology and Mechatronics Automation (ICMTMA), 2011 Third International Conference on, 2011

    The structure of the wing of High Altitude Long Endurance (HALE) Unmanned Aerial Vehicle (UAV) is highly flexible, it's oscillation is obvious and coupled with the flight dynamic responses of the UAV, this influent the flight security seriously. In the stage of conceptual design of a solar UAV, in order to estimate the scheme rapidly and accurately, it is necessary ...

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Periodicals related to Optimal Wing Design

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  • Control Systems Magazine, IEEE

    The magazine covers theory, analysis, design (computer-aided design), and practical implementation of circuits, and the application of circuit theoretic techniques to systems and to signal processing. Content is written for the spectrum of activities from basic scientific theory to industrial applications.

  • Plasma Science, IEEE Transactions on

    Plasma science and engineering, including: magnetofluid dynamics and thermionics; plasma dynamics; gaseous electronics and arc technology; controlled thermonuclear fusion; electron, ion, and plasma sources; space plasmas; high-current relativistic electron beams; laser-plasma interactions; diagnostics; plasma chemistry and colloidal and solid-state plasmas.

  • Robotics, IEEE Transactions on

    Publishes fundamental papers on all aspects of Robotics, featuring interdisciplinary approaches from computer science, control systems, electrical engineering, mathematics, mechanical engineering, and other fields. Robots and intelligent machines and systems are critical in areas such as industrial applications; service and personal assistants; surgical operations; space, underwater, and remote exploration; entertainment; safety, search, and rescue; military applications; agriculture applications; and intelligent ...