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  • Space Bok – Exploring Legged Jumping Locomotion for Space Exploration

    Paper number

    IAC-18,D3,3,10,x44991

    Author

    Mr. Philip Arm, Switzerland, ETHZ

    Coauthor

    Mr. Patrick Barton, Switzerland, ETHZ

    Coauthor

    Mr. Lars Beglinger, Switzerland, ETHZ

    Coauthor

    Mr. Alex Dietsche, Switzerland, ETHZ

    Coauthor

    Mr. Luca Ferrazzini, Switzerland, ETHZ

    Coauthor

    Mr. Elias Hampp, Switzerland, ETHZ

    Coauthor

    Mr. Jan Hinder, Switzerland, ETHZ

    Coauthor

    Mr. Camille Huber, Switzerland, ZHAW – Zurich University of Applied Sciences

    Coauthor

    Mr. David Schaufelberger, Switzerland, ZHAW – Zurich University of Applied Sciences

    Coauthor

    Mr. Felix Schmitt, Switzerland, ETHZ

    Coauthor

    Mr. Benjamin Sun, Switzerland, ETHZ

    Coauthor

    Mr. Radek Zenkl, Switzerland, ETHZ

    Coauthor

    Mr. Boris Stolz, Switzerland, ETHZ

    Coauthor

    Mr. Hendrik Kolvenbach, Switzerland, ETHZ

    Coauthor

    Prof. Marco Hutter, Switzerland, ETHZ

    Year

    2018

    Abstract
    Until now, wheeled locomotion has been the sole form of transportation for robotic exploration on Moon and Mars. While providing high stability and robustness, those systems are limited in their area of operation. Especially in unstructured environments with steep slopes and lose soil, as found on many celestial bodies, wheeled systems reach their limitations.
    In this context, the use of versatile legged robots for space exploration presents a valid solution. The flexibility of legged systems allows exploring areas, which up until now have been out of human and robotic reach. Moreover, legged robots allow for the use of gaits with long flight-phases which prove to be more efficient in low-gravity environments.
    This paper presents the development of Space Bok, a legged jumping robot prototype for space exploration. In the design, the focus of this quadrupedal robot is laid on high efficiency in low-gravity environments. The robot consists of a lightweight carbon main body and four legs with two custom actuators each. Sensing is done using absolute encoders on each actuator and an IMU. 
    The outcome of hardware tests under terrestrial conditions and simulation tests in low-gravity environments are shown and compared to conventional systems.
    Abstract document

    IAC-18,D3,3,10,x44991.brief.pdf

    Manuscript document

    IAC-18,D3,3,10,x44991.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.