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SpaceHopper: A Small-Scale Legged Robot for Exploring Low-Gravity Celestial Bodies

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arxiv 2403.02831 v1 pith:L3U2BCNR submitted 2024-03-05 cs.RO

classification cs.RO
keywords spacehopperrobotbodygravityjumplandinglocomotionlow-gravity
verification ladder T0 review T1 audit T2 compute T3 formal
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We present SpaceHopper, a three-legged, small-scale robot designed for future mobile exploration of asteroids and moons. The robot weighs 5.2kg and has a body size of 245mm while using space-qualifiable components. Furthermore, SpaceHopper's design and controls make it well-adapted for investigating dynamic locomotion modes with extended flight-phases. Instead of gyroscopes or fly-wheels, the system uses its three legs to reorient the body during flight in preparation for landing. We control the leg motion for reorientation using Deep Reinforcement Learning policies. In a simulation of Ceres' gravity (0.029g), the robot can reliably jump to commanded positions up to 6m away. Our real-world experiments show that SpaceHopper can successfully reorient to a safe landing orientation within 9.7 degree inside a rotational gimbal and jump in a counterweight setup in Earth's gravity. Overall, we consider SpaceHopper an important step towards controlled jumping locomotion in low-gravity environments.

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Cited by 2 Pith papers

Reviewed papers in the Pith corpus that reference this work. Sorted by Pith novelty score. Full citation record

  1. Benchmarking Different QP Formulations and Solvers for Dynamic Quadrupedal Walking

    cs.RO 2025-02 conditional novelty 6.0 of 10

    HPIPM with a sparse MPC formulation is the fastest solver, and the Jetson ARM board is the most power-efficient platform according to the new Solve Frequency per Watt metric.

  2. Autonomy in the Real-World: Autonomous Trajectory Planning for Asteroid Reconnaissance via Stochastic Optimization

    physics.space-ph 2024-12 conditional novelty 5.0 of 10

    A stochastic trajectory optimization planner for asteroid reconnaissance produces flyby paths whose simulated observation time under uncertainty exceeds the as-flown OSIRIS-REx trajectory.

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