Friction model of a revolute joint for a precision deployable spacecraft structure

Author:

Hachkowski M. Roman1,Peterson Lee D.2,Lake Mark S.3

Affiliation:

1. Raytheon Optical Systems, Danbury, Connecticut 06810

2. University of Colorado, Boulder, Colorado 80309-0429

3. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Reference25 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. Nonlinear Dynamics of an All-Movable Rudder System with Freeplay Nonlinearity;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2023-03-04

2. Deployable Structures: Structural Design and Static/Dynamic Analysis;Journal of Elasticity;2021-10-27

3. Equivalent Beam Model for Spatial Repetitive Lattice Structures with Hysteretic Nonlinear Joints;International Journal of Mechanical Sciences;2021-06

4. Three-to-one internal resonance in a two-beam structure connected with nonlinear joints;Archive of Applied Mechanics;2021-05-24

5. Parametric Design of Conforming Joints for Thin-Shell Coilable Structures;AIAA Scitech 2019 Forum;2019-01-06

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