The principle of piloted vehicle mechanics is presented, and aircraft longitudinal movement is studied. Assuming that the pilot counters with his lateral controls any sideslip, and that the aircraft plane of symmetry is vertical, the trajectory is described in that same vertical plane. The natural modes (angle of attack oscillation, phugoid, aperiodic motion) of the small movements around straight and level flight, the response to the pilots commands, and equilibrium stability, are examined. Small lateral movements around straight and level flight and the aircraft response to lateral controls are considered. Small movements of the aircraft around stabilized level flight in rotation are also examined. The assumptions of separation of longitudinal and lateral movements around stabilized straight and level flight are validated.


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    Titel :

    Flight Dynamics and Aircraft Piloting


    Beteiligte:
    J. C. Wanner (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    419 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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