Pages that link to "Item:Q3451359"
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The following pages link to Adaptive fault‐tolerant control for feedback linearizable systems with an aircraft application (Q3451359):
Displaying 13 items.
- A unified approach to nonlinear dynamic inversion control with parameter determination by eigenvalue assignment (Q1665977) (← links)
- Active fault tolerant control scheme for aircraft with dissimilar redundant actuation system subject to hydraulic failure (Q1717501) (← links)
- Robust passive adaptive fault tolerant control for stochastic wing flutter via delay control (Q2423963) (← links)
- Adaptive actuator failure compensation for nonlinear MIMO systems with an aircraft control application (Q2470040) (← links)
- Actuator fault-tolerant control (FTC) design with post-fault transient improvement for application to aircraft control (Q2817354) (← links)
- Adaptive fault-tolerant backstepping control against actuator gain faults and its applications to an aircraft longitudinal motion dynamics (Q2857643) (← links)
- Adaptive neural dynamic surface control of MIMO nonlinear time delay systems with time-varying actuator failures (Q2970864) (← links)
- INTEGRATED FAULT TOLERANT FLIGHT CONTROL DESIGN WITH APPLICATION TO AN F-16 AIRCRAFT (Q3099454) (← links)
- (Q3131277) (← links)
- (Q3369238) (← links)
- Multi-rate adaptive control with applications to lateral dynamics of aircraft (Q3748926) (← links)
- Adaptive fault‐tolerant control for a nonlinear flexible aircraft wing system (Q5213932) (← links)
- (Q5282747) (← links)
