This paper presents a project of missile guidance system based on the strapdown guidance technology. The project is composed of strapdown seeker and inertial measurement unit. The integrated guidance and control technology have been adopted. The project raise accuracy of missiles on the premise that the low cost should be guaranteed. According to simulation experiment, this paper proves the feasiblity of the scheme, and it has good ballistic missile.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Research on Missile System with Strapdown Guidance Technology



    Erschienen in:

    Advanced Materials Research ; 785-786 ; 1560-1563


    Erscheinungsdatum :

    04.09.2013


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Strapdown guidance component research

    Hayes, R. J. | NTRS | 1968


    Suboptimal Guidance and Control Design for a Missile with Onboard Strapdown Seeker

    Singh, N. / Sinha, M. | British Library Conference Proceedings | 2012




    Guidance Information Estimation for Strapdown Imaging Seeker of Tactical Missile Guided by Optimal Guidance Law

    Wang, Qi / Liao, Zhizhong / Yan, Fei | British Library Conference Proceedings | 2022