Abstract This paper deals with an optimal placement problem of sensors and actuators for active vibration control of flexible structures. For undamped structures with collocated rate sensors and actuators, two solutions of generalized algebraic Riccati equations (generalized control algebraic Riccati equation, GCARE; generalized filtering algebraic Riccati equation, GFARE) are obtained explicitly. Employing these explicit solutions, we can obtain a stabilizing H∞controller based on the normalized coprime factorization approach without solving any algebraic Riccati equations numerically. Generally, in a optimal sensor/actuator placement problem with a model-based control law (LQG or H∞), the feedback controller needs to be obtained for all candidates of the optimal placement (which may be derived with some numerical optimization techniques) by solving algebraic Riccati equations numerically. Therefore, the amount of computation required to determine the optimal sensor/actuator placement and the controller increases rapidly for large-scale structures which have many pairs of sensor/actuators. The H∞controller in this paper can be obtained just by addition and multiplication of several matrices. Furthermore, a closed-loop property on H∞norm is automatically bounded for all candidates of the optimal placement. Hence, we can formulate the optimal sensor/actuator placement problem to optimize other closed-loop properties (norm of the closed-loop system) with less computational requirement than the model-based method mentioned above. The gradient of the H2norm of the closed-loop system, which is necessary for a descent-based optimization technique, is derived. Using this sensitivity formula, we obtain the optimal placements of two pairs of sensors and actuators which minimize the H2norm of the closed-loop system for a simply supported beam by the quasi-Newton method. The simulation results show the effectiveness of the proposed design method.
[1]
R. Haftka,et al.
An approach to structure/control simultaneous optimization for large flexible spacecraft
,
1987
.
[2]
Keith Glover,et al.
Robust control design using normal-ized coprime factor plant descriptions
,
1989
.
[3]
Koichi Inoue,et al.
The Positioning of Sensors and Actuators in the Vibration Control of Flexible Systems
,
1990
.
[4]
Leonard Meirovitch,et al.
Dynamics And Control Of Structures
,
1990
.
[5]
Singiresu S Rao,et al.
Optimal placement of actuators in actively controlled structures using genetic algorithms
,
1991
.
[6]
Santosh Devasia,et al.
Piezoelectric actuator design for vibration suppression - Placement and sizing
,
1993
.
[7]
Wodek Gawronski,et al.
Actuator and Sensor Placement for Control of Flexible Structures
,
1993
.
[8]
Hitoshi Doki,et al.
Sensor Placement and Model Reduction in Stabilization of Flexible Beams.
,
1993
.
[9]
Akio Nagamatsu,et al.
Integrated Optimum Design of the Structure ad H.INF. Control System Using Genetic Algorithm.
,
1995
.
[10]
Min-Hung Hsiao,et al.
Optimal modal-space controller for structural damping enhancements
,
1995
.
[11]
W. Gawronski,et al.
Balanced actuator and sensor placement for flexible structures
,
1996
.
[12]
Wodek Gawronski.
Actuator and sensor placement for structural testing and control
,
1997
.
[13]
Wodek Gawronski,et al.
Dynamics and Control of Structures
,
1998
.