A novel hybrid robust control design method for F-16 aircraft longitudinal dynamics

DOI10.1155/2020/5281904zbMath1459.93118OpenAlexW3088775567MaRDI QIDQ2004123

Yanyan Li

Publication date: 14 October 2020

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2020/5281904

Mathematics Subject Classification ID

Application models in control theory (93C95) Adaptive control/observation systems (93C40) Automated systems (robots, etc.) in control theory (93C85) Variable structure systems (93B12)

Uses Software

• EDMdeveloperSeat

Cites Work

• Flight control design using non-linear inverse dynamics
• Adaptive nonlinear control without overparametrization
• Backstepping adaptive control of time-varying plants
• A new integral sliding mode design method for nonlinear stochastic systems
• Decentralized sliding-mode control for attitude synchronization in spacecraft formation
• Sliding controller design for non-linear systems
• Design of Robust Control Systems for a Hypersonic Aircraft
• Feedback linearization and backstepping: an equivalence in control design of strict-feedback form

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