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  • IAC-16/C1/2
  • Paper #34987
  • Paper information

    Paper code

    IAC-16,C1,2,5,x34987

    Order

    5

    Room

    Salon Jalisco E6

    Title

    Integrated 6-DOF spacecraft orbit-attitude dynamics modeling and its application in hovering control over an asteroid

    abstract

    View PDF

    Session

    2. Guidance, Navigation & Control (2)

    symposium

    C1. ASTRODYNAMICS SYMPOSIUM

    congress

    IAC-16

    Type of presentation

    oral

    Main author

    Dr. Yue Wang, Beihang University, China