Model Following control for a Light Combat Aircraft

Santharam, A (1988) Model Following control for a Light Combat Aircraft. Project Report. NAL, Bangalore.

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    Abstract

    The design of a candidate control law for LCA to improve longitudinal handling quality by satisfying C* criteria which is a blend of normal acceleration and pitch rate is . addressed The model following control technic used, wherein the pilot input goes through a dynamic C* model and feed forward gains so that the C* of aircraft is forced to follow that of the model in addition to satisfying short period damping and natural frequency requirements . The perfect model following, optimal model following and pole placement technics are used for computing feed back and feed forward gains .

    Item Type: Proj.Doc/Technical Report (Project Report)
    Uncontrolled Keywords: Model Following;Optimal Control;Handling Quality;Active Controls;Control Configured Vehicle
    Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
    AERONAUTICS > Aircraft Stability and Control
    Division/Department: Aerospace Electronics and Controls Division
    Depositing User: Mr Nisanth
    Date Deposited: 16 Jul 2012 11:43
    Last Modified: 16 Jul 2012 11:43
    URI: http://nal-ir.nal.res.in/id/eprint/10575

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