Aiming at the interception problem of the hypersonic aircraft during its coast phase, the Singer Model was used to perform target trajectory prediction based on the early-warning information, and the predicted interception point between the interceptor and the hypersonic target was calculated accordingly. An energy optimal guidance law based on the predicted interception point was designed for the midcourse of the interceptor, and the Uncertain Interval was considered for the existence of various errors to avoid control effort’s oscillations around zero. Simulation experiments are conducted to illustrate the performance of the proposed method.


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    Title :

    Energy Optimal Midcourse Guidance Law Design Based on Predicted Interception Point


    Additional title:

    Lect. Notes Electrical Eng.


    Contributors:
    Yan, Liang (editor) / Duan, Haibin (editor) / Yu, Xiang (editor) / Fang, Yi (author) / Ludan, Li (author) / Yaosheng, Hu (author)


    Publication date :

    2021-10-30


    Size :

    14 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





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