In this paper a novel method to improve the residual vibration suppression in underactuated uncertain flexible systems through motion planning is proposed. The proposed technique relies on the concurrent use of input shaping and on the alteration of the mechanical properties of the system, which enables the enhancement of the robustness to uncertain parameters. Robustness is formulated through the parametric sensitivities of the natural frequencies that provide an analytical and non-probabilistic tool, which is embedded in the eigenstructure assignment algorithm developed in this work. The effectiveness of the proposed method is assessed through a benchmark testbed composed by a triple pendulum attached to a delta robot, that should execute...
Input shaping control techniques have proven to be very effective in improving performance and lower...
© American Society of Mechanical EngineersThe original input shaping technique developed by Singer a...
In this paper, a new approach for vibration control of flexible spacecraft during attitude maneuveri...
Fast motions of systems with constrained flexible dynamics often lead to residual vibrations. Estab...
Abstract: Input Shaping is a widely used method of suppressing residual vibrations in point-to-point...
This paper presents the results of a series of experimental tests carried out on the Space Robot Sim...
This paper presents the results of hybrid vibration controllers applied for vibration suppression of...
International audienceThis paper addresses the problem of reducing the elastic deformations and the ...
Dynamic systems which undergo rapid motion can excite natural frequencies that lead to residual vi...
Input shaping technique is widely used in reducing or eliminating residual vibration of flexible str...
Residual vibrations affect machines at the end of commanded motion and represent an amplification fa...
AbstractThis paper presents a proposal for a minimum energy feedforward control technique for flexib...
This paper aims at investigating vibrational behaviors of the industrial manipulator Racer 7-1.4, de...
The original input shaping technique, that was developed in earlier work, is summarized, and a diffe...
Input shaping is a method for controlling residual vibration in linear systems. Because input shapin...
Input shaping control techniques have proven to be very effective in improving performance and lower...
© American Society of Mechanical EngineersThe original input shaping technique developed by Singer a...
In this paper, a new approach for vibration control of flexible spacecraft during attitude maneuveri...
Fast motions of systems with constrained flexible dynamics often lead to residual vibrations. Estab...
Abstract: Input Shaping is a widely used method of suppressing residual vibrations in point-to-point...
This paper presents the results of a series of experimental tests carried out on the Space Robot Sim...
This paper presents the results of hybrid vibration controllers applied for vibration suppression of...
International audienceThis paper addresses the problem of reducing the elastic deformations and the ...
Dynamic systems which undergo rapid motion can excite natural frequencies that lead to residual vi...
Input shaping technique is widely used in reducing or eliminating residual vibration of flexible str...
Residual vibrations affect machines at the end of commanded motion and represent an amplification fa...
AbstractThis paper presents a proposal for a minimum energy feedforward control technique for flexib...
This paper aims at investigating vibrational behaviors of the industrial manipulator Racer 7-1.4, de...
The original input shaping technique, that was developed in earlier work, is summarized, and a diffe...
Input shaping is a method for controlling residual vibration in linear systems. Because input shapin...
Input shaping control techniques have proven to be very effective in improving performance and lower...
© American Society of Mechanical EngineersThe original input shaping technique developed by Singer a...
In this paper, a new approach for vibration control of flexible spacecraft during attitude maneuveri...