@inproceedings{ec46ad84f082442e80489c052138903a,
title = "Lattice-based discrete structure modeling and control for large flexible space structure applications",
abstract = "This paper introduces a low order spring-mass-damper model of a carbon fiber octahedron voxel, which is used to create a template for a large flexible, light weight, space structure. The proposed template is used to develop a decentralized linear matrix inequality (LMI) based control design for suppressing structural vibrations subjected to both output and control input constraints. The proposed structural model consists of active voxels (with control authority) and passive voxels (without control authority). The performance of various quantities of active voxels are compared using the developed control approach.",
author = "Nick Cramer and Swei, {Sean S.M.} and Cheung, {Kenneth C.} and Daniel Cellucci and Benjamin Jenett and Mircea Teodorescu",
note = "Funding Information: This research is funded in part by NASA AMRD Convergent Aeronautics Solutions (CAS) project and in part by UARC NAS2-03144 project. Publisher Copyright: {\textcopyright} 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017 ; Conference date: 09-01-2017 Through 13-01-2017",
year = "2017",
doi = "10.2514/6.2017-1981",
language = "British English",
isbn = "9781624104534",
series = "58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017",
booktitle = "58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017",
}