A path following control architecture that drives a gliding missile, that is a missile without thrust, toward a prespecified linear path in an inertial frame using only torque control is developed and flight results are presented. A fast time-scale inner-loop control system stabilizes the orientation dynamics with a custom control law. Two slow time-scale outer-loop designs are proposed that render the inertial path exponentially stable for the missile’s translational dynamics. Since a gliding missile has no thrust input, the outer-loop is unable to directly actuate its control. Instead, we present an orientation extraction scheme to convert the outer-loop’s control signal into a desired orientation for the inner-loop. The control algorithm is implemented on a proprietary missile and empirical flight data are presented to demonstrate its effectiveness.


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    Titel :

    Path Following Control Design for a Gliding Missile


    Beteiligte:


    Erscheinungsdatum :

    2022-02-01


    Format / Umfang :

    1468630 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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