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  • Preliminary Experimental Results of Beam Steering Control Subsystem for Solar Power Satellite

    Paper number

    IAC-12,C3,2,4,x14557

    Author

    Dr. Takehiro Miyakawa, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Daisuke Joudoi, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Masanobu Yajima, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Prof. Susumu Sasaki, Japan Aerospace Exploration Agency (JAXA)/ISAS, Japan

    Coauthor

    Mr. Takuro Sasaki, Mitsubishi Electric Corporation, Japan

    Coauthor

    Dr. Yukihiro Homma, Mitsubishi Electric Corporation, Japan

    Year

    2012

    Abstract
    Solar Power Satellite (SPS) converts the space solar energy into microwave or laser, and transmits it to the earth. The SPS in the geostationary orbit can collect the power at any time of the day and night, and transmit gigawatts of power to a power receiving subsystem on the earth. To achieve 1GW-class SPS, a power transmitting subsystem on the scale of square kilometers is required for microwave power transmission (MPT). Consequently, it is crucial to construct a number of transmitting modules in the power transmitting subsystem, and transmit microwave beams pointing accurately to power receiving subsystem. To achieve MPT technology, the Japan Aerospace Exploration Agency and the Institute for Unmanned Space Experiment Free Flyer are planning to conduct a MPT ground experiment in fiscal year 2014. In this joint effort, we are in charge of a beam steering control (BSC) subsystem, which is important among MPT technologies. We have defined the functions and specifications of the BSC Breadboard Models (BBMs). Using the BBMs of the BSC subsystem, we conduct the functional verification of a REV method and a monopulse method. We have two test items. First, we check the detection of the arrival angle of the pilot signal. At a tracking receiver, we receive the “sum” and “difference” signals derived from the pilot signal,  and pass an angle error signal to a CPU card. Then, we confirm that phase control signal which comes from the CPU card is correct. Second, we confirm that phase differences which are set initially are corrected for three transmitting modules using the REV method. This paper describes the functions and specification of the BSC BBMs, the results of system tests for BSC BBMs.
    Abstract document

    IAC-12,C3,2,4,x14557.brief.pdf

    Manuscript document

    IAC-12,C3,2,4,x14557.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.