Multiple model predictive control for large envelope flight of hypersonic vehicle systems
- 1 January 2016
- journal article
- Published by Elsevier BV in Information Sciences
- Vol. 328, 115-126
- https://doi.org/10.1016/j.ins.2015.08.033
Abstract
No abstract availableKeywords
Funding Information
- National Nature Science Foundation of China (61374109, 61304078, 61473184)
- National Basic Research Program of China (973 Program-2013CB035500)
- High Technology Research and Development Program of China (2015AA043102)
This publication has 35 references indexed in Scilit:
- Robust tracking control for an air-breathing hypersonic vehicle with input constraintsInternational Journal of Systems Science, 2013
- Stability of switched positive linear systems with average dwell time switchingAutomatica, 2012
- Multimodel Control of Nonlinear Systems: An Integrated Design Procedure Based on Gap Metric and H∞ Loop ShapingIndustrial & Engineering Chemistry Research, 2012
- Adaptive Kriging controller design for hypersonic flight vehicle via back-steppingIET Control Theory & Applications, 2012
- Neural network-based robust control for hypersonic flight vehicle with uncertainty modellingInternational Journal of Modelling, Identification and Control, 2010
- Multi-model predictive control method for nuclear steam generator water levelEnergy Conversion and Management, 2007
- Multi-model predictive control based on the Takagi–Sugeno fuzzy models: a case studyInformation Sciences, 2004
- Gap Metric Concept and Implications for Multilinear Model-Based Controller DesignIndustrial & Engineering Chemistry Research, 2003
- Min-max feedback model predictive control for constrained linear systemsIEEE Transactions on Automatic Control, 1998
- Optimal robustness in the gap metricIEEE Transactions on Automatic Control, 1990