The task of this work is to design the guidance system for themissile which would guide the missile accurately to hit the target asdirected. Guidance is the main component of the missile system whichhelps in hitting the target accurately. The missile can be guided bythe number of ways which includes by using laser, GPS infrared orradio waves on its way to the target. This paper proposes a model toguide the missile with the help of GPS and INS. This model requires acomputer or controller which should be installed in the missile tocontrol the missile flight according to the guidance provided by GPSand INS. The system works by knowing the missile current positionand the position of the target. The position of the target is known byusing Google maps which is feed in the missile controller before themissile is launched. Missile current position is known by using GPSwhile the missile current orientation and heading is known by usingINS. Missile current position is compared with the target position tocalculate the desired heading towards the target, then missilecontroller auto pilots the missile according to the desired headingtowards target to hit the target.


    Access

    Download


    Export, share and cite



    Title :

    GPS Inertial Missile Guidance System


    Contributors:

    Publication date :

    2015-10-14


    Remarks:

    Pakistan Journal of Engineering, Technology & Science; Vol 4, No 2 (2014) ; 2224-2333 ; 2222-9930



    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    DDC:    629



    Sliding Mode and Inertial Delay Control Based Missile Guidance

    Phadke, S. B. / Talole, S. E. | IEEE | 2012


    Strategic Interferometric Fiber-Optic Gyroscope for Ballistic Missile Inertial Guidance

    Divakaruni, S. / Keith, G. / Narayanan, C. et al. | British Library Conference Proceedings | 2008


    Strategic Interferometric Fiber-Optic Gyroscope for Ballistic Missile Inertial Guidance

    Divakaruni, Sudhakar / Keith, Gregg / Narayanan, Chellappan et al. | AIAA | 2008


    A High Reliability Solid State Accelerometer for Ballistic Missile Inertial Guidance

    Becka, S. / Novack, M. / Slivinsky, S. et al. | British Library Conference Proceedings | 2008


    A High Reliability Solid State Accelerometer for Ballistic Missile Inertial Guidance

    Becka, Steve / Novack, Mitchell / Slivinsky, Sandra et al. | AIAA | 2008