Research on RBV control strategy of large angle maneuver

DOI10.1155/2014/718125zbMath1406.93176OpenAlexW2013125892WikidataQ59040873 ScholiaQ59040873MaRDI QIDQ1724808

Yu Fu, Xiande Wu, Na Luo, Jiangtao Xu, Litong Wang

Publication date: 14 February 2019

Published in: Abstract and Applied Analysis (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2014/718125

zbMATH Keywords

hypersonic aerospace vehiclelarge angle maneuverRBV controlrobust adaptive dynamic inversion

Mathematics Subject Classification ID

Sensitivity (robustness) (93B35) Learning and adaptive systems in artificial intelligence (68T05) Application models in control theory (93C95) Adaptive control/observation systems (93C40) Control/observation systems governed by ordinary differential equations (93C15)

Cites Work

• \(H_\infty \) model reduction for uncertain switched linear discrete-time systems
• Nonlinear control law with application to high angle-of-attack flight
• Stable adaptive tracking of uncertain systems using nonlinearly parametrized on-line approximators
• Dynamic inversion: an evolving methodology for flight control design
• Gain-scheduled bank-to-turn autopilot design using linear parameter varying transformations
• $l_{2}-l_{\infty}$ Model Reduction for Switched LPV Systems With Average Dwell Time
• Stability, ${l}_{2}$-Gain and Asynchronous ${H}_{{\infty}}$ Control of Discrete-Time Switched Systems With Average Dwell Time

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