DocumentCode :
1015830
Title :
Fault-tolerant joint development for the Space Shuttle remote manipulator system: analysis and experiment
Author :
Wu, Eugene C. ; Hwang, James C. ; Chladek, John T.
Author_Institution :
NASA/Johnson Space Center, Lockheed Eng. & Sci. Co., Houston, TX, USA
Volume :
9
Issue :
5
fYear :
1993
fDate :
10/1/1993 12:00:00 AM
Firstpage :
675
Lastpage :
684
Abstract :
The feasibility of space-based fault-tolerant robot joint design with a dual-motor, single-output differential-based mechanical drive system is investigated. The mathematical model of the differential system is developed, and the inherent nonlinear dynamic characteristics for the differential are reduced to linear state equations through variable substitutions. Nonlinear phenomena such as gearbox forward/backdrive efficiency, motor friction/stiction, and torque limiting are included. Simulations have been performed for various joint failure conditions. A scaled-down differential testbed has been designed and built to validate the analytical results. Simulation and test results demonstrate that the design is capable of sustaining a single failure and absorbing the failure disturbance, and continuing to be operational with the remaining single drive mode
Keywords :
dynamics; friction; kinematics; manipulators; space vehicles; telecontrol; dual-motor single-output differential-based mechanical drive system; failure disturbance; gearbox forward/backdrive efficiency; linear state equations; motor friction/stiction; nonlinear dynamic characteristics; space shuttle remote manipulator system; space-based fault-tolerant robot joint design; torque limiting; Differential equations; Fault tolerance; Fault tolerant systems; Friction; Mathematical model; Nonlinear dynamical systems; Nonlinear equations; Orbital robotics; Space shuttles; Testing;
fLanguage :
English
Journal_Title :
Robotics and Automation, IEEE Transactions on
Publisher :
ieee
ISSN :
1042-296X
Type :
jour
DOI :
10.1109/70.258058
Filename :
258058
Link To Document :
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