TL;DR: In this article, a boundary-element model was used to identify a regional slip vector of N275°E, which suggests that the plate configuration assumed by previous workers must be modified and a new configuration is proposed that remains consistent with the data used for earlier interpretations and their new data.
Abstract: When a region is tectonically deformed, its geometry changes. Some of these changes produce easily identified and often readily datable morphological features such as regions of rapid uplift and subsidence, sediment ponds, or river terraces. These features are usually secondary to the main active structures and consequently do not provide information about them directly. We show, however, that simple models using boundary-element methods can be adapted to relate the evolution of these minor features to motion on major structures. This adds substantially to the information available to determine motion on such features. In this paper, we apply the technique to northwest Greece. We show that, in addition to the long recognized compressional component of motion in Epirus, a substantial left-lateral strike-slip component of motion must be present. The modeling allows us to identify a regional slip vector of N275°E. This slip vector suggests that the plate configuration assumed by previous workers must be modified. A new configuration is proposed that remains consistent with the data used for earlier interpretations and our new data. It is proposed that the Medina Wrench is a significant active structure and that a period of quiescence explains the low seismic activity at present. The plate configuration and angular rotation rates that we suggest require that the Gulf of Arta is associated with a triple junction. Using the slip vectors we have defined for the plates meeting at this junction, we model the regions of uplift and subsidence in the region. The ability of this model to explain many features associated with the Gulf provides assurance that our overall tectonic model is correct.
TL;DR: In this paper, an approach for the design of active piezoelectric fins developed for a small-scale flight vehicle is presented using analytical and computational tools that are based on the high-order theory and provide a graphical representation of the response spectrum of the active fin.
Abstract: A systematic approach for the design of active piezoelectric fins developed for a small-scale flight vehicle is presented. The proposed design approach uses analytical and computational tools that are based on the high-order theory and provides a graphical representation of the response spectrum of the active fin. In addition, it enables the coupling of the structural and aerodynamic analyses and provides a frame in which the results of the two types of analysis are adjoined. A numerical design study of a twist-actuated smart fin is presented and discussed. The results reveal the sensitivity of the structure to a broad range of geometrical, mechanical, and electromechanical design variables and provide guidelines for the optimization of the active structure. A set of normalized design master curves that can be scaled to fit various geometrical layouts of the structure investigated are also presented and discussed.
TL;DR: In this study, two cascade optimization procedures are performed to assess the best positioning and velocity feedback gains of the actuators that must be controlled to damp vibrations of the mesh deployable reflector.
TL;DR: In this paper, the authors describe recent advances in structural quieting technology as applied to active truss structures intended for high precision space-based optics applications, where piezoelectric active members exert control forces internal to the structure and thereby improve the structure's dimensional stability.
Abstract: This paper describes recent advances in structural quieting technology as applied to active truss structures intended for high precision space based optics applications. The active structure incorporates piezoelectric active members which exert control forces internal to the structure and thereby improve the structure's dimensional stability. The control architecture involves two layers of feedback control. The first utilizes collocated measurements of force and velocity at the active member to achieve active damping, the second utilizes noncollocated measurements of acceleration at the location of a simulated optical component to achieve structural stabilization. The local control loops are based on the concept of impedance matching, the global control loops are designed using robust control methods. These two levels of control are intended to operate simultaneously; however, in this paper each approach is applied individually. The combined implementation is left for future work.
TL;DR: In this paper, the authors considered the control of an active flexible structure by examin ing the equations of motion of an integrated actuator/structure system containing both the actuator and structure dynamics.
Abstract: The slewing control of an active flexible structure is considered by examin ing the equations of motion of an integrated actuator/structure system containing both the actuator and structure dynamics. These equations are derived using a Hamiltonian ap proach. The system under consideration is a slewing flexible structure, a thin aluminum beam, torque driven by an armature controlled DC electric motor and actuated by a piece- wise distributed piezoceramic actuator. An improvement in performance is gained by 1) including the effects of motor actuator and beam dynamic interaction and 2) using a piezo electric device, layered on the structure, for direct vibration suppression of the structural dynamics. A comparison is made using simulations, to point out the advantages of slewing an active structure versus slewing a passive structure. This presents a multi input slewing control problem which is implemented using a standard linear quadratic regulator control design.