Computer-Aided Detection and Characterization of Micro-Dynamic Responses of a Large Deployable Precision Structure

Author:

Babuska Vit1,Erwin R. Scott2,Moser Ruth2

Affiliation:

1. Veridian Systems

2. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. Lake, M.S. and M.R. Hatchkowski, "Design of Mechanisms for Deployable Optics Instruments: Guidelines for Reducing Hysteresis," NASA TM Jan2000.

2. Microdynamic behavior of a joint dominated structure on-orbit

3. Hardaway, L. and L.D. Peterson, " Stability and Mechanics of Precision Deplyable Structures Under Nanometer Deformation," University of Colorado Report CU-CAS-00-12, Boulder CO, May2000.

4. Experimental control of microdynamic events observed during the testing of a large deployable optical structure

5. Warren, P.A. and L.D. Peterson, "Sub-Micron Non-Linear Shape Mechanics of Precision Deployable Structures," University of Colorado Report CU-CAS-96-18, Boulder CO, July1996.

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