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    Paper code

    IAC-17,C1,4,4,x41530

    Date

    2017-09-27

    Time

    09:45

    Order

    4

    Room

    Hall A

    Title

    Ascent Flight Control of Launch Vehicle Using Angle of Attack Estimator

    abstract

    View PDF

    Session

    4. Guidance, Navigation & Control (2)

    symposium

    C1. ASTRODYNAMICS SYMPOSIUM

    congress

    IAC-17

    Type of presentation

    oral

    Main author

    Mr. Ario Birmiawan Widyoutomo, The Graduate Universty for Advanced Studies (SOKENDAI), Japan

    Co-authors

    Prof. Yasuhiro Morita, Japan Aerospace Exploration Agency (JAXA), Japan;