Adaptive sliding mode attitude tracking control for flexible spacecraft systems based on the Takagi-Sugeno fuzzy modelling method
Authors:
- Ang LiALAng Li
- Ming LiuMLMing Liu
- Yan ShiYSYan Shi
- 1 October 2020
- journal article
- research article
- Published by Elsevier in Acta Astronautica
- Vol. 175, 570-581
Abstract
No abstract availableKeywords
Funding Information
- National Key Research and Development Program of China (2016YFB0500901)
- National Natural Science Foundation of China (61690212, 61833009, 91438202)
This publication has 35 references indexed in Scilit:
- Time-shared scheme design for attitude control system during space separationAerospace Science and Technology, 2011
- A linear matrix inequality approach to robust fault detection filter design of linear systems with mixed time-varying delays and nonlinear perturbationsJournal of the Franklin Institute, 2010
- New methodologies for adaptive sliding mode controlInternational Journal of Control, 2010
- Higher order sliding mode control based on integral sliding modeAutomatica, 2007
- Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuverAerospace Science and Technology, 2005
- Output stabilization of flexible spacecraft with active vibration suppressionIEEE Transactions on Aerospace and Electronic Systems, 2003
- Adaptive Nonlinear Control of Multiple Spacecraft Formation FlyingJournal of Guidance, Control, and Dynamics, 2000
- On stability of fuzzy systems expressed by fuzzy rules with singleton consequentsIEEE Transactions on Fuzzy Systems, 1999
- New methods to design an integral variable structure controllerIEEE Transactions on Automatic Control, 1996
- Attitude Control of a Flexible SpacecraftJournal of Guidance and Control, 1980