MIMO-FEA Active Vibration Suppression of a Satellite Using an Adaptive Composite Thruster Platform

Aerospace ◽  
2006 ◽  
Author(s):  
Mehrdad N. Ghasemi-Nejhad ◽  
Nicolas Antin

Adaptive or intelligent structures which have the capability for sensing and responding to their environment promise a novel approach to satisfying the stringent performance requirements of future space missions. This research focuses on a finite element analysis (FEA) multi-input-multi-output (MIMO) approach for vibration suppression and precision position control of a satellite thruster and its structure, due to the thruster-firing, employing an intelligent composite thruster platform. This smart platform connects the thruster to the structure of the satellite and has three active struts and one active central support with piezoelectric stacks as actuators, and each has a sensor at its base. It also has an active circular composite plate as the top device plate with nine embedded piezoelectric patches that six of them are back-to-back and function as three actuators pairs and three of them are placed next to the bottom actuators and function as sensors. Here, the predominant modes of the structure are first determined. In the FEA method, a finite element harmonic analysis was employed to develop a vibration suppression scheme, which was then used to study the vibration control of the satellite structure using the vibration suppression capabilities of the intelligent platform mounted on the satellite. In this approach, the responses of the structure to a unit external force as well as unit internal piezoelectric control voltages are first determined, individually. The responses are then assembled in a system of equation as a coupled system and then solved simultaneously to determine the control voltages and their respective phases for the system actuators for a given external disturbance. Next, this technique was applied to the vibration suppression of the satellite frame as well as its thruster simultaneously as a coupled problem and the results are discussed. This approach is an effective technique for the design of smart structures with complex geometry to study their active vibration suppression capabilities and effectiveness. The entire system has ten actuators: four piezoelectric stack actuators and three pairs of piezoelectric patch actuators.

Aerospace ◽  
2006 ◽  
Author(s):  
Mehrdad N. Ghasemi-Nejhad ◽  
Randy Sakagawa

Adaptive structures combine sensors, actuators, and control systems for intelligent responses to their environment and promise a novel approach to satisfying the stringent performance requirements of future aerospace and space applications. This study focuses on a multi-input-multi-output finite element analysis for the design and active vibration suppression of an adaptive circular composite plate used here as the top device-plate for an intelligent composite platform that is designed for thrust vector control of a satellite thruster. The adaptive circular composite plate has three pairs of back-to-back embedded piezoelectric active fiber composite actuator patches. A finite element harmonic analysis is employed to develop a vibration suppression scheme, which is then used to study the vibration suppression of the circular composite plate using the piezoelectric patches embedded in the plate. In this approach, the responses of the structure to an arbitrary external force as well as an arbitrary internal piezoelectric control voltage are first determined, individually. Using the linearity of the system, the responses are then assembled in a system of equation as a coupled system and then solved simultaneously to determine the control voltages and their respective phases for the system actuators for a given external disturbance. This approach is an effective technique for the design of smart structures with complex geometry and multi-input-multi-output sensor and actuator systems to study their active vibration suppression capabilities and effectiveness. The design and active vibration suppression of the adaptive circular composite plate are explained and discussed.


2010 ◽  
Vol 148-149 ◽  
pp. 934-937
Author(s):  
Xiu Mei Wang ◽  
Ju Zheng Wang ◽  
Xiao Jin Zhu

Active vibration control based on fuzzy algorithm for piezoelectric smart plate is studied. After the characteristic of piezoelectric ceramic (PZT) is analyzed, modal and transient analysis are developed in this paper with finite element model of the piezoelectric smart plate constructed in ANSYS. Fuzzy logic control rules are established by the analysis of the deformation of the plate. With mode shape and displacement response curve obtained, active vibration suppression for the smart plate system is achieved by using commercial finite element programs. The simulation results illustrate that analysis of piezoelectric smart plate using ANSYS is practicable and the intelligent control method is effective.


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