An active disturbance rejection guidance and control scheme for homing missiles with three-dimensional impact angle constraints is proposed. The six-degree-of-freedom dynamical and kinematical models containing model uncertainties and disturbances are established. A strict feedback relative dynamics between the target and homing missile in three-dimensional space are deduced. A reconstructed reduced-order attitude controller design model is proposed. A two-loop control structure with respect to the centroid guidance loop and rotational control loop is conducted to implement the six-degree-of-freedom guidance and control system with the help of second-order sliding mode approach and extended state observers. The tracking loop of the Euler angles of the missile can be elided and the number of six-degree-of-freedom control parameters can be reduced. Finally, the effectiveness and robustness of the newly proposed guidance and control scheme are investigated and verified via six-degree-of-freedom nonlinear simulation studies.


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    Titel :

    Active disturbance rejection guidance and control scheme for homing missiles with impact angle constraints


    Beteiligte:
    Wang, Jian Hua (Autor:in) / Cai, Yuan Wen (Autor:in) / Cheng, Long (Autor:in) / Li, Yan (Autor:in) / Jun Xin, Chao (Autor:in) / Xie, Wei Qi (Autor:in) / Tang, Guo Jian (Autor:in)


    Erscheinungsdatum :

    2019-03-01


    Format / Umfang :

    14 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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