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  • Rendezvous Technique of HTV and Evaluation of On-orbit Results

    Paper number

    IAC-11,C1,9,2,x11033

    Author

    Mr. Nobuharu Kambara, Mitsubishi Electric Corporation, Japan

    Coauthor

    Mr. Masaharu Suzuki, Mitsubishi Electric Corporation, Japan

    Coauthor

    Mr. Daisuke Watabe, Mitsubishi Electric Corporation, Japan

    Coauthor

    Mr. Masahide Onji, Mitsubishi Electric Corporation, Japan

    Coauthor

    Dr. Shoji Yoshikawa, Mitsubishi Electric Corporation, Japan

    Coauthor

    Dr. Hirohiko Uematsu, JAXA, Japan

    Coauthor

    Mr. Toru Kasai, Japan Aerospace Exploration Agency (JAXA), Japan

    Coauthor

    Mr. Satoshi Ueda, Japan Aerospace Exploration Agency (JAXA), Japan

    Year

    2011

    Abstract
    The H-II Transfer Vehicle (HTV) “KOUNOTORI” developed by Japan Aerospace Exploration Agency (JAXA) is an automated unmanned cargo transport system to the International Space Station (ISS).  The HTV mission is to supply requisite materials according to the international agreement among the ISS partners, and therefore the HTV is required to arrive at the ISS as scheduled.  On the other hand, strict safety requirements are applied to the HTV so that even in the case of a catastrophic failure, the HTV can automatically abort the rendezvous flight and escape from the vicinity of the ISS.  These apparently-opposing requirements raised a lot of technical challenges in the development process of the HTV Guidance, Navigation and Control (GN&C) system.  However, they were overcome by well-balanced design of guidance and control logic, navigation system including sensors and safety management functions, such as Fault Detection, Isolation and Recovery (FDIR).  The design was verified by various test methods to show the compliance with the requirements.  This paper introduces evaluation of the HTV GN&C system design as a function that takes a major role of Rendezvous technique, based on the result of the HTV 1st and 2nd flights. Especially, design solution and on-orbit flight data evaluation regarding the requirements are focused to show how these technical difficulties were resolved.
    Abstract document

    IAC-11,C1,9,2,x11033.brief.pdf

    Manuscript document

    IAC-11,C1,9,2,x11033.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.