On the coupled dynamics of small spacecraft and elastic deployable appendages
From MaRDI portal
Publication:2014684
DOI10.1007/s11044-016-9524-9zbMath1376.70002OpenAlexW2440519313MaRDI QIDQ2014684
S. M. Malaek, P. Bagheri Ghaleh, Alireza Abedian
Publication date: 25 August 2017
Published in: Multibody System Dynamics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s11044-016-9524-9
Cites Work
- Dynamics modeling and analysis of a flexible-base space robot for capturing large flexible spacecraft
- Dynamic analysis of an axially translating viscoelastic beam with an arbitrarily varying length
- Unified multi-domain modelling and simulation of space robot for capturing a moving target
- Hamiltonian dynamic analysis of an axially translating beam featuring time-variant velocity
- Parametric response of cantilever Timoshenko beams with tip mass under harmonic support motion
- Vibration and stability of an axially moving Rayleigh beam
- On the dynamics of an axially moving beam
- Dynamics of wire boom oscillations on a spinning satellite part I, lagrangian equations of motion and transient response
- Dynamics of wire boom oscillations on a spinning satellite part II, normal modes in spin plane
- Periodic behavior of a cantilever beam with end mass subjected to harmonic base excitation
- Modeling of flexible beams for robotic manipulators
- On the choice of boundary conditions for mode shapes in flexible multibody systems
- 3D DYNAMIC ANALYSIS OF A FLEXIBLE DEPLOYING ARM SUBJECTED TO BASE ANGULAR MOTIONS
- INVESTIGATION OF IN-ORBIT DISTURBING LOADS INDUCED ON SPACECRAFT DUE TO ELASTIC DEPLOYING ARM
- A general formulation for librational dynamics of spacecraft with deploying appendages
This page was built for publication: On the coupled dynamics of small spacecraft and elastic deployable appendages
