• DocumentCode
    3031331
  • Title

    Allocation and optimization for performance indexes of the flight control system based on equivalent system matching

  • Author

    Liu Zhijun ; Gao Yakui

  • Author_Institution
    Autom. Sch., Northwestern Polytech. Univ., Xi´an, China
  • fYear
    2013
  • fDate
    20-22 Dec. 2013
  • Firstpage
    3701
  • Lastpage
    3704
  • Abstract
    Performance parameters are the basis of a system design. The optimum performance of the subsystems not always assembles to obtain the optimum performance of the main system. So it´s necessary to allocate and optimize the index parameters. This paper firstly introduced definition of the index-allocator which was used to allocate the index parameters of the systems. And the nonlinear programming method was firstly used to allocate and optimize damping ratio and control bandwidth of the flight control system based on the low order equivalent system. In the meantime, the impact of the allocation results on the control accuracy was considered. Simulations verify that the allocation approach is reasonable and feasible.
  • Keywords
    aerospace control; damping; least squares approximations; nonlinear programming; performance index; control accuracy; control bandwidth; damped least square method; damping ratio optimization; equivalent system matching; flight control system; index parameter allocation; index parameter optimization; low order equivalent system; nonlinear programming method; performance index; performance parameters; system design; Accuracy; Aerospace control; Bandwidth; Damping; Optimization; Performance analysis; Resource management; equivalent system; index-allocator; indexes allocation and optimization; nonlinear programming;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
  • Conference_Location
    Shengyang
  • Print_ISBN
    978-1-4799-2564-3
  • Type

    conf

  • DOI
    10.1109/MEC.2013.6885640
  • Filename
    6885640