4.6 Article

Reactive Landing Controller for Quadruped Robots

Journal

IEEE ROBOTICS AND AUTOMATION LETTERS
Volume 8, Issue 11, Pages 7210-7217

Publisher

IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC
DOI: 10.1109/LRA.2023.3313919

Keywords

Legged robots; quadrupedal robots; robot control

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In this letter, the authors propose an optimization-based reactive Landing Controller for torque-controlled quadruped robots in free-fall. The method utilizes an estimate of the Center of Mass horizontal velocity and a Variable Height Springy Inverted Pendulum model to continuously recompute the feet position for a successful landing in all directions.
Quadruped robots are machines intended for challenging and harsh environments. Despite the progress in locomotion strategy, safely recovering from unexpected falls or planned drops is still an open problem. It is further made more difficult when high horizontal velocities are involved. In this letter, we propose an optimization-based reactive Landing Controller that uses only proprioceptive measures for torque-controlled quadruped robots that free-fall on a flat horizontal ground, knowing neither the distance to the landing surface nor the flight time. Based on an estimate of the Center of Mass horizontal velocity, the method uses the Variable Height Springy Inverted Pendulum model for continuously recomputing the feet position while the robot is falling. In this way, the quadruped is ready to attain a successful landing in all directions, even in the presence of significant horizontal velocities. The method is demonstrated to dramatically enlarge the region of horizontal velocities that can be dealt with by a naive approach that keeps the feet still during the airborne stage. To the best of our knowledge, this is the first time that a quadruped robot can successfully recover from falls with horizontal velocities up to $3 \ \mathrm{m/s}$ in simulation. Experiments prove that the used platform, Go1, can successfully attain a stable standing configuration from falls with various horizontal velocities and different angular perturbations.

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