Energy Storage System Control for Energy Management in Advanced Aeronautic Applications

被引:9
作者
Cavallo, A. [1 ]
Canciello, G. [1 ]
Guida, B. [1 ]
机构
[1] Second Univ Napoli, Dept Ind & Informat Engn, I-81031 Aversa, Italy
关键词
All Open Access; Gold;
D O I
10.1155/2017/4083132
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
In this paper an issue related to electric energy management on board an aircraft is considered. A battery pack is connected to a high-voltage bus through a controlled Battery Charge/Discharge Unit (BCDU) that makes the overall behaviour of the battery "intelligent." Specifically, when the aeronautic generator feeding the high-voltage bus has enough energy the battery is kept under charge, while if more loads are connected to the bus, so that the overload capacity of the generator is exceeded, the battery "helps" the generator by releasing its stored energy. The core of the application is a robust, supervised control strategy for the BCDU that automatically reverts the flow of power in the battery, when needed. Robustness is guaranteed by a low-level high gain control strategy. Switching from full-charge mode (i.e., when the battery absorbs power from the generator) to generator mode (i.e., when the battery pumps energy on the high-voltage bus) is imposed by a high-level supervisor. Different from previous approaches, mathematical proofs of stability are given for the controlled system. A switching implementation using a finite-time convergent controller is also proposed. The effectiveness of the proposed strategy is shown by detailed simulations in Matlab/Stateflow/SimPowerSystem.
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页数:9
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共 22 条
  • [1] [Anonymous], P 8 INT C POW EL MAC
  • [2] Limit cycles in control systems employing smart actuators with hysteresis
    Cavallo, A
    Natale, C
    Pirozzi, S
    Visone, C
    [J]. IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2005, 10 (02) : 172 - 180
  • [3] Cavallo A, 2015, IEEE DECIS CONTR P, P4734, DOI 10.1109/CDC.2015.7402957
  • [4] Cavallo A, 2012, IEEE DECIS CONTR P, P7088, DOI 10.1109/CDC.2012.6427026
  • [5] Active vibration control by a smart auxiliary mass damper equipped with a fiber Bragg grating sensor
    Cavallo, Alberto
    May, Chris
    Minardo, Aldo
    Natale, Ciro
    Pagliarulo, Pietro
    Pirozzi, Salvatore
    [J]. SENSORS AND ACTUATORS A-PHYSICAL, 2009, 153 (02) : 180 - 186
  • [6] Ding SH, 2015, IEEE DECIS CONTR P, P4752, DOI 10.1109/CDC.2015.7402960
  • [7] Aircraft power systems: Technology, state of the art, and future trends
    Emadi, A
    Ehsani, M
    [J]. IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 2000, 15 (01) : 28 - 32
  • [8] Faleiro L., P 25 C INT COUNC AER
  • [9] Ghosh S., 2012, Electrical Machines
  • [10] Guida B., 2013, P IEEE 18 INT C EM T