Results from the synthesis of control laws for an advanced short takeoff aircraft in a low-speed approach flight condition are given. Two of four candidate synthesis techniques are reported: direct eigenspace assignment and explicit model following via a linear quadratic regulator (LQR) formulation. A fundamental objective of this work is to obtain low-order feedback compensators, synthesized via the above techniques, and the judicious use of state estimation, thus allowing the use of a reasonable number of sensors for feedback.


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    Titel :

    Multi-input multi-output system control for experimental aircraft


    Beteiligte:

    Erscheinungsdatum :

    20.08.1987


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch