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  • study of heater electric power control with autonomous distributed control

    Paper number

    IAC-17,D1,3,6,x40115

    Author

    Mr. Keisuke Umeda, The University of TOKYO, Graduate school, Japan

    Coauthor

    Mr. Yusuke Oki, Department of Engineering ,The University of Tokyo, Japan

    Coauthor

    Dr. Takanao Saiki, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Dr. Osamu Mori, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Dr. Junichiro Kawaguchi, Japan Aerospace Exploration Agency (JAXA), Japan

    Year

    2017

    Abstract
    Spacecrafts have many heaters. When many heaters turn on at the same time, the total power consumption of system also gets large and then there is a possibility that the power resource runs short. Therefore, it is important to distribute the power to each heater appropriately and control the power consumption of heater.
    
    HAYABUSA mission adopted “Server client system. ”A server was installed and controlled allocation of electric power by communicating with each heater. However, there were some problems. First, when the number of heaters gets large, the time to communicate with heaters also gets large. Second, it is impossible to test the control unless all devices are available. Therefore, it takes a long time to develop a spacecraft.
    Third, since a plurality of high-cost servers are required, the cost is very large to combine redundancy.
    
    In order to solve the problems, this paper proposes"Autonomous distributed system." In this system, a transmitter is located instead of a server. Each heater calculates its own power allocation with the information which the transmitter broadcasts. By using this system, even if the number of heaters gets large, the time to communicate does not change, and short-time control is possible. Besides, as the transmitter only broadcasts the total power consumption and each heater does not have to know the states of other heaters, the test of the control algorithm can be performed separately
    and the time to develop a spacecraft can be shortened. Moreover, it does not need an expensive server.
    
    In this system, each heater determines whether to turn on or off based on the Eq.(\ref{eq:Heater Control})
    \begin{eqnarray}
    \label{eq:Heater Control}
    C_{i,k+1}=C_{i,k}-$\Delta$P_k\times\frac{1}{Q_i}
    \end{eqnarray}
    Where \begin{math}i\end{math} is a heater number, \begin{math}k\end{math} is a step number, \begin{math}C\end{math} is the variable which represents the state of a heater, \begin{math}$\Delta$P\end{math} is the difference between the target value and total power consumption, and \begin{math}Q\end{math} is the priority of a heater. Each heater judges whether or not to turn on based on whether \begin{math}C\end{math} is larger than the threshold value or not.
    
    This paper demonstrates that it is possible to control power consumption and temperature of heaters by both a simulation and an experiment. Comparing these two results verifies the utility of this control scheme. In the experiment, ZigBee, which is a wireless unit, is used to broadcast from the transmitter to the heaters.
    Abstract document

    IAC-17,D1,3,6,x40115.brief.pdf

    Manuscript document

    IAC-17,D1,3,6,x40115.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.