T-S fuzzy modelling and \(H_{\infty}\) attitude control for hypersonic gliding vehicles
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Publication:1993004
DOI10.1155/2017/6574527zbMath1426.93167OpenAlexW2618021272WikidataQ59147699 ScholiaQ59147699MaRDI QIDQ1993004
Xianlin Huang, Xiao-Zhi Gao, Wei-Dong Zhang
Publication date: 5 November 2018
Published in: Mathematical Problems in Engineering (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1155/2017/6574527
Fuzzy control/observation systems (93C42) (H^infty)-control (93B36) Control of mechanical systems (70Q05)
Cites Work
- An efficient approach for reducing the conservatism of LMI-based stability conditions for continuous-time T-S fuzzy systems
- Fuzzy dynamic characteristic model based attitude control of hypersonic vehicle in gliding phase
- LMI approach to analysis and control of Takagi-Sugeno fuzzy systems with time delay
- Stability analysis and design of fuzzy control systems
- s-norm aggregation of infinite collections
- Analysis and design of fuzzy control system
- Analytical methods in fuzzy modeling and control
- Robust adaptive neural control of flexible hypersonic flight vehicle with dead-zone input nonlinearity
- Dynamic output feedback control of a flexible air-breathing hypersonic vehicle via T–S fuzzy approach
- Reducing the conservatism of LMI-based stabilisation conditions for TS fuzzy systems using fuzzy Lyapunov functions
- Analysis and synthesis of discrete nonlinear passive systems via affine T–S fuzzy models
- Robust tracking control for an air-breathing hypersonic vehicle with input constraints
- Universal fuzzy controllers for a class of nonlinear systems
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