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Development of the dynamic motion simulator of 3D micro-gravity with a combined passive/active suspension systemThe establishment of those in-orbit operations like 'Rendez-Vous/Docking' and 'Manipulator Berthing' with the assistance of robotics or autonomous control technology, is essential for the near future space programs. In order to study the control methods, develop the flight models, and verify how the system works, we need a tool or a testbed which enables us to simulate mechanically the micro-gravity environment. There have been many attempts to develop the micro-gravity testbeds, but once the simulation goes into the docking and berthing operation that involves mechanical contacts among multi bodies, the requirement becomes critical. A group at the Tokyo Institute of Technology has proposed a method that can simulate the 3D micro-gravity producing a smooth response to the impact phenomena with relatively simple apparatus. Recently the group carried out basic experiments successfully using a prototype hardware model of the testbed. This paper will present our idea of the 3D micro-gravity simulator and report the results of our initial experiments.
Document ID
19950017291
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yoshida, Kazuya
(Tokyo Inst. of Tech. Tokyo, Japan)
Hirose, Shigeo
(Tokyo Inst. of Tech. Tokyo, Japan)
Ogawa, Tadashi
(Tokyo Inst. of Tech. Tokyo, Japan)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Publication Information
Publication: JPL, Third International Symposium on Artificial Intelligence, Robotics, and Automation for Space 1994
Subject Category
Ground Support Systems And Facilities (Space)
Accession Number
95N23711
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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