We want to intercept an airborne target, or a target on the surface with a homing missile. The missile has a seeker and an attitude control system. There is a platform, such as a ship, which has a radar to track the missile and the target. This platform possibly launches the missile. We will discuss two parts of the intercept guidance problem: midcourse guidance and terminal guidance. In midcourse guidance the target is not in the field of view of the missile, since they are too far apart. In terminal guidance, the target is in the field of view of the missile seeker.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Missile Guidance For Intercept


    Contributors:
    D. Serakos (author)

    Publication date :

    2021


    Size :

    42 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Missile guidance with constrained intercept body angle

    Rusnak, Ilan / Weiss, Haim / Eliav, Rei et al. | IEEE | 2014


    Optimal Intercept Missile Guidance Strategies with Autopilot Lag

    Chen, R. / Speyer, J. / Lianos, D. et al. | British Library Conference Proceedings | 2010


    Hybrid Guidance Laws for Improved Missile Intercept Ranges

    Broadston, R. / Hutchins, Robert / Titus, H. et al. | AIAA | 2002


    Optimal Intercept Missile Guidance Strategies with Autopilot Lag

    Chen, Robert / Speyer, Jason / Lianos, Dimitrios | AIAA | 2010


    Optimal Intercept Missile Guidance Strategies with Autopilot Lag

    Chen, Robert H. / Speyer, Jason L. / Lianos, Dimitrios | AIAA | 2010