Evaluation of inertial devices for the control of large, flexible, space-based telerobotic armsBatch simulation studies which show that torque-wheels can reduce the overshoot in abrupt stop commands by 82 percent for a two-link arm are presented. For man-in-the-loop evaluation, a real-time simulator has been developed that samples a hand-controller, solves the nonlinear equations of motion, and graphically displays the resulting motion on a computer workstation. It is shown that, for a single-link arm, a reaction-mass/torque-wheel combination at the payload end can yield a settling time of 3 s for disturbances in the first flexible mode as opposed to 10 s utilizing only a hub motor.
Document ID
19930034713
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Montgomery, Raymond C. (NASA Langley Research Center Hampton, VA, United States)
Kenny, Sean (NASA Langley Research Center Hampton, VA, United States)
Ghosh, Dave (NASA Langley Research Center Hampton, VA, United States)
Shenhar, Joram (Lockheed Engineering and Sciences Co. Hampton, VA, United States)