62 / 2016-03-01 09:10:39
A new type of missile fuzzy controller design and simulation
9461,9462,9463
全文录用
李 颖 / 南昌航空大学
Abstract:the missile in flight with a non-linear,coupled and time-varying ,in addition,the flight parameters have rapid changed,the traditional PID control can not meet the requirements of dynamic control.Aiming at this problems,in this paper put forward a kind of effective method to control missile attitude, improve the controllability of the missile control system.As missile pitch channel for an example,Based on the PID fuzzy control theory,designed a parallel fuzzy PID controller,and given the relationship about controller and the coefficients KP, KI, KD of the conventional PID controller .The simulation results show that the scheme has good stability, effectively reducing the amount of regulation time and the system overshoot.
重要日期
  • 会议日期

    07月08日

    2016

    07月10日

    2016

  • 04月25日 2016

    终稿截稿日期

  • 05月20日 2016

    初稿截稿日期

  • 07月10日 2016

    注册截止日期

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