CubeSats Passive Control Vibration Isolation Analysis Using Transfer Matrix Method
- 1 August 2017
- conference paper
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- p. 91-96
Abstract
Vibration effects for space crafts has a great influence during the launching phase and also after launching. Active vibration isolation techniques have good results to protect such systems from vibration problems in wide frequency bands. But, these active systems increase the total weight of space craft. That will increase the need of power supplies, which may affect the mission life time due to batteries and solar cell charging consuming. Passive control for such problem is designed using Transfer Matrix Method for Multibody Systems (MSTMM) that can provide an easy method to analyze a passive vibration isolation technique with simple design. The main objective of this paper is to study the different models effect in isolation design using MSTMM and passive control techniques to conserve the power consumption for enlarging the power batteries life. That means longer mission intervals for such systems. Simulation results are given to demonstrate the effectiveness of the offered technique.Keywords
This publication has 10 references indexed in Scilit:
- Transfer matrix method for determination of the natural vibration characteristics of elastically coupled launch vehicle boostersActa Mechanica Sinica, 2015
- Modeling computational limitations in H-Phy and Overlay-NoC architecturesThe Journal of Supercomputing, 2013
- CubeSat: The Pico-Satellite Standard for Research and Education2008
- Review of Active Techniques for Aerospace Vibro-Acoustic ControlJournal of Aircraft, 2002
- Survey of Active Vibration Isolation Systems for Microgravity ApplicationsJournal of Spacecraft and Rockets, 2000
- Vibration analysis of one-dimensional structures using the spectral transfer matrix methodEngineering Structures, 2000
- Whole-spacecraft vibration isolation system for the GFO/Taurus mission1999
- Proposition of an incremental transfer matrix method for nonlinear vibration analysis.JSME International Journal. Ser. 3, Vibration, Control Engineering, Engineering for Industry, 1991
- Critical requirements for the design of large space structures1981
- Vibration and Noise Problems Expected in Manned Space CraftNoise Control, 1959