Shape Control of Inflatable Reflectors

Author:

Utku S.1,Kuo C. P.,Garba J. A.,Wada B. K.2

Affiliation:

1. Department of Civil and Environmental Engineering, Box 90287, Duke University, Durham, NC 27708-0287

2. Jet Propulsion Laboratory, Pasadena, CA 91109

Abstract

In this work studied are the means of maintaining the target design geometry of inflatable membranes that are used for low frequency antenna collectors. Considering the deviations from the target state as the linear combinations of a set of given n normalized undesirable displacement patterns (e.g., Fourier-Zernike functions), the linearized thin shell and membrane theories are used to obtain expressions for the components of the corresponding n number of induced macro strain states. Then the problems associated with the failure in implementing by piezofilm actuators all the components of the geometrically compatible macro strain states are studied. As a result of these studies several recommendations are given.

Publisher

SAGE Publications

Subject

Mechanical Engineering,General Materials Science

Reference12 articles.

Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. 6.17 Shape Control of Composites;Comprehensive Composite Materials II;2018

2. Distributed and Localized Active Vibration Isolation in Membrane Structures;Journal of Spacecraft and Rockets;2006-09

3. Active Vibration Suppression Strategy for a Membrane Reflector/Mirror Undergoing Slewing Maneuvers;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

4. Distributed Localized Vibration Control of Membrane Structures Using Piezoelectric Actuators;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18

5. Investigation of Geometric Imperfection in Inflatable Aerospace Structures;Journal of Aerospace Engineering;2004-07

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