There is a renewed interest in dynamic characteristics of damaged aircraft both in order to assess survivability and to develop control laws to enhance survivability. This paper presents a set of flight dynamics equations of motion for a rigid body not necessarily referenced to the body's center of mass. Such equations can be used when the body loses a portion of its mass and it is desired to track the motion of the body s previous center of mass/reference frame now that the mass center has moved to a new position. Furthermore, results for equations presented in this paper and equations in standard aircraft simulations are compared for a scenario involving a generic transport aircraft configuration subject to wing damage.


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    Titel :

    General Equations of Motion for a Damaged Asymmetric Aircraft


    Beteiligte:
    B. J. Bacon (Autor:in) / I. M. Gregory (Autor:in)

    Erscheinungsdatum :

    2007


    Format / Umfang :

    13 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    General Equations of Motion for a Damaged Asymmetric Aircraft

    Bacon, Barton / Gregory, Irene | AIAA | 2007


    General Equations of Motion for a Damaged Asymmetric Aircraft

    Bacon, Barton J. / Gregory, Irene M. | NTRS | 2007


    General Equations of Motion for a Damaged Asymmetric Aircraft AIAA Paper

    Bacon, B. / Gregory, I. | British Library Conference Proceedings | 2007


    DYNAMIC INVERSE RESILIENT CONTROL OF A DAMAGED ASYMMETRIC GENERAL AVIATION AIRCRAFT

    Arruda, M. / Steck, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010