• DocumentCode
    3205129
  • Title

    Reliable design for MPPT management through the SMP technique

  • Author

    Schirone, Luigi ; Macellari, Michele ; Schiaratura, Alfiero

  • Author_Institution
    Dipt. di Ing. Aerospaziale e Astronautica, Univ. degli Studi di Roma La Sapienza, Rome
  • fYear
    2009
  • fDate
    7-14 March 2009
  • Firstpage
    1
  • Lastpage
    9
  • Abstract
    Operation of a S/C power system based on the SMP technique for Maximum Power Point Tracking management is the subject of the present work. Improvements both in transient behaviour and EMC are reported and experimental results are analysed with reference to specific design solutions. Particular design techniques are then presented, specifically developed to avoid that the increased circuit complexity could negatively affect the system reliability, especially in the cases where Commercial Off The Shelf components are used. Basically, the circuits for fundamental operation, designed on the basis of classical and very reliable schemes, are separated from those dedicated to the SMP control, based on digital integrated circuits, with an higher failure rate. Then, the interfaces between the two blocks are designed so that the SMP control circuit can only affect (positively) the system operation when it is correctly operating, while its interactions with the basic circuit are blocked if errors are detected.
  • Keywords
    aircraft power systems; power system control; power system reliability; switched mode power supplies; MPPT management; SMP control circuit; SMP technique; maximum power point tracking management; Complexity theory; Digital control; Electromagnetic compatibility; Energy management; Integrated circuit reliability; Power system analysis computing; Power system management; Power system reliability; Power system transients; Transient analysis;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace conference, 2009 IEEE
  • Conference_Location
    Big Sky, MT
  • Print_ISBN
    978-1-4244-2621-8
  • Electronic_ISBN
    978-1-4244-2622-5
  • Type

    conf

  • DOI
    10.1109/AERO.2009.4839521
  • Filename
    4839521