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Hiroki Kato

6 accepted papers

2020

Subsurface Sampling Robot for Time-limited Asteroid Exploration

IROS 2020poster

This paper presents a novel approach to sampling subsurface asteroidal regolith under severe time constraints. Sampling operations that must be completed within a few hours require techniques that can manage subsurface obstructions that may be encountered. The large uncertainties due to our lack of…

Cited by 7SourceScholar
2019

Contact-Event-Triggered Mode Estimation for Dynamic Rigid Body Impedance-Controlled Capture

ICRA 2019poster

This paper presents a contact-event-triggered filter using only a force-torque sensor with impedance control for non-cooperative, rotating, heavy object capture. Contact events are modeled for prediction, and detected to trigger the particle filter's updating process. By combining these features, a…

Cited by 3SourceScholar
2018

Online Path Planning and Compliance Control of Space Robot for Capturing Tumbling Large Object

IROS 2018poster

This paper presents the path planning and coordinated control of a space robot with a manipulator for capturing a rotating large object. As the grasping point on a rotating large object is translationally moving fast, an appropriate strategy and coordinated motion control of the spacecraft base and…

Cited by 18SourceScholar
2017

Caging-based grasp with flexible manipulation for robust capture of a free-floating target

ICRA 2017poster

This paper discusses robust capture of a free-floating target using a robotic arm. The position error resulting from sensor errors and time delay can cause undesired contact and unstable control. In this paper, we propose a caging-based rigid gripper and impedance control, which enables the robot to…

Cited by 28SourceScholar
2017

Distance control of rocket-propelled miniature exploration robot

ICRA 2017poster

A rocket-propelled miniature robot is capable to explore sites that planetary rovers cannot reach with efficiency in locomotion distance per mass. The technical difficulty is the significant variance in its flight distance because of two factors: sensitivity of error in the center of gravity with re…

Cited by 4SourceScholar