DocumentCode :
425042
Title :
Interconnection and damping assignment passivity-based control of mechanical systems with underactuation degree one
Author :
Acosta, J.A. ; Ortega, Romeo ; Astolfi, Alessandro
Author_Institution :
Dept. de Ingenieria de Sist. y Aut., Seville Univ., Spain
Volume :
4
fYear :
2004
fDate :
June 30 2004-July 2 2004
Firstpage :
3029
Abstract :
We consider the problem of (asymptotic) stabilization of mechanical systems with underactuation degree one. A state-feedback design is derived applying the interconnection and damping assignment passivity-based control methodology. Its application relies on the possibility of solving a set of partial differential equations that identify the energy functions that can be assigned to the closed-loop. The following results are established: 1) identification - in terms of some algebraic inequalities - of a subclass of these systems for which the partial differential equations are trivially solved; 2) characterization of all systems which are feedback-equivalent to this subclass; and 3) introduction of a suitable parametrization of the assignable energy functions that provides the designer with a handle to address transient performance and robustness issues. An additional feature of our developments is that the open-loop system need not be described by a port-controlled Hamiltonian (or Lagrangian) model, a situation that arises often in applications due to model reductions or preliminary feedbacks that destroy the structure. The new result is applied to obtain an (almost) globally stabilizing controller for the inertia wheel pendulum, a controller for the chariot with pendulum system that can swing-up the pendulum from any position in the upper half plane and stop the chariot at any desired location, and an (almost) globally stabilizing scheme for the vertical takeoff and landing aircraft with strong input coupling. In all cases we obtain very simple and intuitive solutions that do not rely on, rather unnatural and technique-driven, linearization or decoupling procedures but instead endows the closed-loop system with a Hamiltonian structure with desired potential and kinetic energy functions.
Keywords :
aircraft landing guidance; asymptotic stability; closed loop systems; control system synthesis; damping; identification; inertial systems; nonlinear control systems; open loop systems; partial differential equations; pendulums; state feedback; Lagrangian model; aircraft landing; aircraft vertical takeoff; algebraic inequalities; asymptotic stabilization; chariot controller; closed loop system; damping assignment passivity control; identification; inertia wheel pendulum system; interconnection control; kinetic energy functions; open loop system; partial differential equations; port controlled Hamiltonian model; potential energy functions; state feedback design; underactuated mechanical systems;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 2004. Proceedings of the 2004
Conference_Location :
Boston, MA, USA
ISSN :
0743-1619
Print_ISBN :
0-7803-8335-4
Type :
conf
Filename :
1384373
Link To Document :
بازگشت