Estimation and regulation of the rate of convergence of a rigid robot to a set-point with applications to spacecraft attitude control

  • Authors:
  • Amit Ailon;Michael I. Gil;Rogelio Lozano

  • Affiliations:
  • Department of Electrical and Computer Engineering, Ben Gurion University of the Negev, P.O. Box 653, Beer Sheva 84105, Israel;Department of Mathematics, Ben Gurion University of the Negev, Beer Sheva 84105, Israel;Université de Technologie de Compiègne, URA C.N.R.S. 817, BP 649, 60206 Compiègne Cédex, France

  • Venue:
  • Nonlinear Analysis: Real World Applications
  • Year:
  • 2003

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Abstract

This study presents an explicit upper bound to the norm of the solution of the equation of motion of an n-degree of freedom rigid robot while it is under the action of a PD controller. The resulting upper bound is an exponential function that reflects the effect of the controller gains on the form of the system response. The relevant procedure is applicable also in the case of model uncertainty. A tuning-rule for setting the controller gains and adjusting the system rate of convergence towards the desired operating point has been established. As shown, the effect of the tuning-rule on the resulting upper bound is similar to the one obtained in the case of an appropriate second-order linear system. The applications of the results obtained for a rigid robot model are considered in the framework of the spacecraft attitude control problem. In particular, the present approach might be useful for estimating the rate of convergence and evaluating the region of attraction with respect to a required attitude set-point in the domain of validity of the selected transformation associated with the kinematic representation.