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The power system • Solar arrays • Batteries • Solar array regulators • Distribution system • Secondary power system 4 ,QWURGXFWLRQ WR 6SDFH (OHFWURQLFV 7KH 3RZHU 6XEV\VWHP

3 8 Almacenamiento Paneles Fotovoltaicos

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almacenamiento de paneles fotovoltaicos

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  • The power system

    Solar arrays

    Batteries

    Solar array regulators

    Distribution system

    Secondary power system

    4

  • The power system

    Function: to provide electrical power to all the units on board

    Energy is taken from the sun by the solar arrays

    Then it is processed and distributed to the units

    Exceeding energy is stored in batteries for the eclipse periods

    A secondary conversion might be needed at unit level

    Overview

    The power system is autonomous

  • The power system

    DC/DCCL

    CL

    CL

    CL

    CL

    Solar Array

    Battery

    SAR

    AOCS

    Comms

    DHS

    Motors

    FPGA

    Main Power Bus

    Distribution Lines Payloads

    DC/DC

    DC/DC

    DC/DC

    DC/DC

    A typical configuration could be:

    Primary power system

    Distribution system

    Secondary power system

  • The power system Solar Arrays

    In the majority of satellites the power is generated by solar cells.

    There are several types:

    Silicon

    GaAs

    Multi-junction

    Nowadays, the most used solar cell is the triple junction GaAs cell.

    GaInP

    GaInAs

    Ge

    The conversion efficiency is currently 28%

    The near future target is 30%

  • The power system Solar Arrays

  • The power system Solar Arrays

  • The power system Solar Arrays

  • The power system Solar Arrays

    The I-V curve of a solar cell is as follows:

    It can be defined with three points: Open circuit (OC), Short-circuit (SC) and Maximum Power Point (MPP)

    Depending on the operating point, it can behave as a:

    Current source

    Voltage source

    Cur

    rent

    [A]

    Power curve

  • The power system Solar Arrays

    The I-V curve changes with temperature

    0 1 2 30

    0.5

    1

    1.5

    Voltage [V]

    Cur

    rent

    [A]

    @28 degC@88 degC

    IMPP

    The power available is higher at lower temperatures

    The Voc changes significantly. This is very important for the power converter connected to the SA.

  • The power system Solar Arrays

    It can be mathematically modelled as follows:

    RS = cells series resistance I = generated currentRSH = cells shunt resistance V = cell operation voltageIL = photovoltaic current across junction k = Boltzmanns constant (1.38 E-23 J/K)Io = reverse saturation current of ideal diode T = absolute temperatureI = generated current q = electronic charge (1.6E-19 coulombs)V = cell operation voltage A = curve fitting factor between 1 and 2ID = Io * exp[q*V / (A*k*T)] -1 (combined from 2 terms with A=1 for diffusion current and

    A=2 for recombination current)

    0 1SV I Rq SA k T

    LSH

    V I RI I I e

    R

  • The power system Solar Arrays

    It can also be modelled using the following four parameters:

    VOC ISC VMPP IMPP

    ln 1

    1 1mp cell mp

    sc mp oc

    I v V

    I V Vmpcell sc

    sc

    Ii I e

    I

  • The power system Solar Arrays

    Thermal model

    Temperature is a key parameter to determine the I-V curve and the available power.

    The temperature dependence is assumed to be linear.

    The equilibrium point can be calculated as follows:

    Tfront

    Tback

    Pabsorbed Pemitted_front

    Pemitted_back

    Pelectrical_outRth Cth

    _ _

    _

    1frontabs em f em b out

    panel

    front back th em b

    dTP P P P

    dt C

    T T R P

  • The power system Solar Arrays

    Degradation

    Radiation has provokes degradation on the solar cell performance

    After 15 years in GEO, the performance will be approximately 88%compared to BOL.

    The effects on the voltage and the current parameters are different

    UV also degrades the performance of the cover glass

    Micrometeorites impacts obviously degrade the performance as well

    A fleck of paint left this crater on the surface of Space Shuttle Challenger's front window on STS-7.

  • The power system Solar Arrays

    How are the solar cells arranged to form a solar array?

    The basic idea is to combine a number of them in series [n] to form a string

    And then to connect a number of strings in parallel [m] so that:

    The voltage level and current capability can cope with the demand foreseen

    1

    2

    n

    2 m

  • The power system Solar Arrays

    To improve reliability, protection diodes are added:

    A diode is added in series with each string

    And another one in parallel with each cell

    Otherwise, a short in one string will short the array To avoid that the less

    illuminated cell biases the current of the string

  • Section 1

    SADM

    Section 2

    Section k

    Satellite body

    The power system Solar Arrays

    The strings are arranged in sections

    SADM: solar array drive mechanism

    The SADM has a limited number of lines that can go through

  • The power system Solar Arrays

    Solar cell parasitics

    The most important parasitic is the cell capacitance.

    It is non linear and depends on the voltage and the temperature

    In triple junction cells it is in the order of 1uF

    Note that if the cell was switching, there will be relatively high losses on the switching device