Pages that link to "Item:Q602646"
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The following pages link to Nonlinear \(H_\infty\) robust control applied to F-16 aircraft with mass uncertainty using control surface inverse algorithm (Q602646):
Displaying 5 items.
- Sliding mode attitude tracking of rigid spacecraft with disturbances (Q1933433) (← links)
- A novel hybrid robust control design method for F-16 aircraft longitudinal dynamics (Q2004123) (← links)
- Attitude tracking of rigid spacecraft with actuator saturation and fault based on a compound control (Q2217844) (← links)
- Adaptive integral-sliding-mode control strategy for maneuvering control of F16 aircraft subject to aerodynamic uncertainty (Q2242759) (← links)
- A nonlinear dynamic inversion-based neurocontroller for unmanned combat aerial vehicles during aerial refuelling (Q2877522) (← links)
