Active Vibration Control of Satellite Flexible Structures during Attitude Maneuvers

Abstract

The purpose of this study is controlling active vibration of satellite flexible structures during attitude maneuvers. A smart structure is a structure which is able to sense and control active reaction to any external factors and stimulation. As it comes from the definition of smart structures, development of this knowledge depends on the materials science development, theories and strategies for control. In materials science, smart materials are developed in such a way that they are able to sense and react in a controllable mode effectively. The smart materials are combined with conventional structures and they are used as sensors and actuators. Furthermore, smart structures subject include design, implementation methods and control systems over structures so that the control system receives signals from sensors after processing. Then, it sends signals to the actuator in order to achieve a desirable response to incoming stimuli. An issue taken into account in this monograph is active vibration control of satellite flexible structures in attitude maneuvers, which was done by the use of smart materials in satellite structure. For this purpose, a mathematical model of a satellite flexible panel was derived first. Then, a computer code was generated. Finally, by comparing the results of non-smart control and smart control, we came to this conclusion that the use of smart materials led to a decrease in the amplitude of the vibration and the reduction of the time required for damping vibrations.

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“…brations. Under normal circumstances, big satellites are equipped with active vibration control system, a means of attenuating unwanted on-board vibrations, as an alternative to passive vibration absorbers[7,[121][122][123][124]. The basic principle of the active vibration control lies in a negative feedback system, of which the operation diagram is described inFig.…”

“…The basic principle of the active vibration control lies in a negative feedback system, of which the operation diagram is described inFig. 2.25[122]. Sensors are placed to detect the vibrations, and send the vibration signals to the controller; followed by the controller would cause the actuator to produce vibration responses to enhance the system stability.In Ref.…”

“…[7], a pair of piezoelectric sensor and piezoelectric actuator are used to compensate for the vibrations. When a disturbance occurs, the piezoelectricFigure 2.25: Operation principle of an active vibration control system[122].…”

“…For instance, nano-satellites are miniature satellites that typically only keep the weight around 1∼20 kg, and total power capacity approximately 20∼50 Watt, thus a conventional active vibration control system might be not feasible under these constraints. Recently, smart structures and materials are reported to be suitable to the small-size satellites[122].…”