Pages that link to "Item:Q2814009"
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The following pages link to Application of \(H_{2}/H_\infty\) technique to aircraft landing control (Q2814009):
Displaying 8 items.
- Application of the method of optimized delta-transformations in the control landing problem for an unmanned aerial vehicle (Q2173813) (← links)
- Disturbance encountered landing system design based on sliding mode control with evolutionary computation and cerebellar model articulation controller (Q2282697) (← links)
- (Q2762547) (← links)
- Control parameter tuning for aircraft crosswind landing via multi-solution particle swarm optimization (Q5058811) (← links)
- Autonomous Adaptive Control System for Airplane Landing (Q5215179) (← links)
- New Upper Matrix Bounds with Power Form for the Solution of the Continuous Coupled Algebraic Riccati Matrix Equation (Q5270481) (← links)
- An improved NSGA-II based control allocation optimisation for aircraft longitudinal automatic landing system (Q5382588) (← links)
- Antisaturation fixed-time backstepping fuzzy integral sliding mode control for automatic landing of fixed-wing unmanned aerial vehicles (Q6669329) (← links)