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Cites:

Information Journal Paper

Title

MISSILE AUTOPILOT DESIGN USING FUZZY GAIN-SCHEDULING

Pages

  59-68

Abstract

 In this paper a controller using FUZZY GAIN-SCHEDULING for the channels of a tactical missile is designed such that in flight trajectories, performance is achieved. In this design method, the FUZZY GAIN-SCHEDULING zone centers are determined by a training algorithm according to dynamic pressure, Mach number and coefficients of linear model of system in major operating points. The fuzzy system is learned using combined genetic and LINEAR LEAST SQUARES algorithms. In this manner both global optimum solution and fast convergence are reachable. Moreover the membership functions in fuzzy inference system are chosen with special and suitable properties, which cause simple and effective scheduling process. Performance of this method is shown with case study simulation result.

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  • Cite

    APA: Copy

    AKBAR ZADEH KALAT, A., & MOUMENI, HAMID REZA. (2007). MISSILE AUTOPILOT DESIGN USING FUZZY GAIN-SCHEDULING. NASHRIYYAH-I MUHANDESI-I BARQ VA MUHANDESI-I KAMPYUTAR-I IRAN (PERSIAN), 5(2), 59-68. SID. https://sid.ir/paper/53818/en

    Vancouver: Copy

    AKBAR ZADEH KALAT A., MOUMENI HAMID REZA. MISSILE AUTOPILOT DESIGN USING FUZZY GAIN-SCHEDULING. NASHRIYYAH-I MUHANDESI-I BARQ VA MUHANDESI-I KAMPYUTAR-I IRAN (PERSIAN)[Internet]. 2007;5(2):59-68. Available from: https://sid.ir/paper/53818/en

    IEEE: Copy

    A. AKBAR ZADEH KALAT, and HAMID REZA MOUMENI, “MISSILE AUTOPILOT DESIGN USING FUZZY GAIN-SCHEDULING,” NASHRIYYAH-I MUHANDESI-I BARQ VA MUHANDESI-I KAMPYUTAR-I IRAN (PERSIAN), vol. 5, no. 2, pp. 59–68, 2007, [Online]. Available: https://sid.ir/paper/53818/en

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