A cutoff insensitive guidance scheme is proposed for strategic missile systems not equipped with thrust termination systems. The main idea behind this scheme is to manipulate the current flight-path angle to follow the required flight-path angle. For this, a routine to obtain the required flight-path angle is set up by reorganizing the equations comprising the Lambert routine. Compared with existing schemes, the proposed scheme is more robust to motor performance uncertainty; it is also simpler and has a lighter calculation load. It is shown that the algorithm has good performance through the computer simulation.


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    Titel :

    Flight-Path Angle Control for Cutoff Insensitive Guidance


    Beteiligte:
    Kim, Sang-Jae (Autor:in) / Um, Tae-Yoon (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.04.2015




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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