Al-Tememe transform in solving developed missile automatic control problem

  • Authors

    • Emad Kuffi Al-Mansour University Collage, Communication Engineering Department, Iraq, Baghdad
    • Elaf Sabah Abbas Al-Mansour University Collage, Communication Engineering Department, Iraq, Baghdad
    • Salman Obeid Mebayet Al-Mansour University Collage, Communication Engineering Department, Iraq, Baghdad
    https://doi.org/10.14419/ijet.v7i4.28919

    Received date: April 21, 2019

    Accepted date: June 13, 2019

    Published date: June 30, 2019

  • Al-Tememe Transform, Developed Missile Automatic Control Problem, Second Order Ordinary Differential Equations with Variable Coefficients, Torque, Angle of Error, Moment of Inertia, Angular Velocity.

  • Abstract

    Al-Tememe transform is a new transform that is recently emerged, as a result to its modernity, it has not exploited properly in many applications. Missile automatic control problem is an application of the second order ordinary differential equation with constant coefficients, for that reason many methods in solving second order ordinary differential equations had been used in solving that problem, however, Al-Tememe transform had never been used in solving the problem of missile automatic control. In this paper Al-Tememe transform has been used to solve the developed problem of missile automatic control, which is an application of the second order ordinary differential equations with variable coefficients.

  • References

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  • How to Cite

    Kuffi, E., Sabah Abbas, E., & Obeid Mebayet, S. (2019). Al-Tememe transform in solving developed missile automatic control problem. International Journal of Engineering and Technology, 7(4), 6565-6567. https://doi.org/10.14419/ijet.v7i4.28919