Nonlinear \(H_\infty\) robust control applied to F-16 aircraft with mass uncertainty using control surface inverse algorithm

DOI10.1016/j.jfranklin.2008.05.002zbMath1201.93037OpenAlexW1993607586MaRDI QIDQ602646

Chien-Chun Kung

Publication date: 5 November 2010

Published in: Journal of the Franklin Institute (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.jfranklin.2008.05.002

zbMATH Keywords

robustprefiltercontrol surface inverse algorithmnonlinear \(H_\infty\) control

Mathematics Subject Classification ID

Feedback control (93B52) Nonlinear systems in control theory (93C10) Application models in control theory (93C95) (H^infty)-control (93B36)

Related Items (3)

Sliding mode attitude tracking of rigid spacecraft with disturbances ⋮ Attitude tracking of rigid spacecraft with actuator saturation and fault based on a compound control ⋮ A nonlinear dynamic inversion-based neurocontroller for unmanned combat aerial vehicles during aerial refuelling

Cites Work

• Flight control design using non-linear inverse dynamics
• L/sub 2/-gain analysis of nonlinear systems and nonlinear state-feedback H/sub infinity / control
• Disturbance attenuation and H/sub infinity /-control via measurement feedback in nonlinear systems
• Nonlinear H/sub ∞/ control and its application to rigid spacecraft
• Nonlinear predictive control of feedback linearizable systems and flight control system design
• Spacecraft Euler parameter tracking of large-angle maneuvers via sliding mode control
• Nonlinear H-infinity optimal control for agile missiles

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