12 research outputs found

    Design and analysis of a digitally controlled integrated flight/firecontrol system

    No full text

    Unstable systems database: A new tool for students, teachers and scientists

    Get PDF
    The contribution presents a starting project of a site focused on unstable systems. It is a web-based database in the bilingual version (ENG/CZ) which can be used as an information database for models of unstable processes. The site contains mathematical models of such systems including their simulation files together with basic information about stability of dynamical systems. The paper outlines motivation for development of this database, presents its basic structure and discusses several models from the site. Areas of prospective usage are also suggested together with possible directions of further development of this project. © Springer International Publishing Switzerland 2013

    Model reduction of a nonlinear rocket control system

    No full text

    Stability and Control Properties of an Aeroelastic Fixed Wing Micro Aerial Vehicle

    No full text
    Micro aerial vehicles have been the subject of considerable interest and development over the last several years. The majority of current vehicle concepts rely on rigid fixed wings or rotors. An alternate design based on an aeroelastic membrane wing concept has also been developed that has exhibited desired characteristics in flight test demonstrations and competition. This paper presents results from a wind tunnel investigation that sought to quantify stability and control properties for a family of vehicles using the aeroelastic design. The results indicate that the membrane wing does exhibit potential benefits that could be exploited to enhance the design of future flight vehicles
    corecore