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    Conceptual Design Optimization of an Augmented Stability Aircraft Incorporating Dynamic Response and Actuator Constraints (AIAA 2014-0187)

    Conceptual Design Optimization of an Augmented Stability Aircraft Incorporating Dynamic Response and Actuator Constraints (AIAA 2014-0187)


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    Titel :

    Conceptual Design Optimization of an Augmented Stability Aircraft Incorporating Dynamic Response and Actuator Constraints (AIAA 2014-0187)

    Beteiligte:
    Welstead, J. (Autor:in) / Crouse, G.L. (Autor:in) / American Institute of Aeronautics and Astronautics
    Kongress:

    52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD

    Erschienen in:

    Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 1809-1830

    PAPERS- AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS ; 3

    Erscheinungsdatum :

    2014-01-01

    Format / Umfang :

    22 pages

    Anmerkungen:

    Includes bibliographical references and author index

    ISBN :

    9781632669285

    Medientyp :

    Aufsatz (Konferenz)

    Format :

    Print

    Sprache :

    Englisch

    Schlagwörter :

    AIAA , Aerospace sciences , Aeronautics , Astronautics

    © Metadata Copyright the British Library Board and other contributors. All rights reserved.

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