Pages that link to "Item:Q2821192"
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The following pages link to Automatic control of aircraft in lateral-directional plane during landing (Q2821192):
Displaying 11 items.
- Disturbance encountered landing system design based on sliding mode control with evolutionary computation and cerebellar model articulation controller (Q2282697) (← links)
- Automatic landing of a civil aircraft with the use of ground landmarks (Q2457145) (← links)
- Synthesis of automatic control for plane-type UAV landing and stability analysis of desired motion regimes (Q2657170) (← links)
- (Q2762547) (← links)
- Application of \(H_{2}/H_\infty\) technique to aircraft landing control (Q2814009) (← links)
- Landing Auto-Pilots for Aircraft Motion in Longitudinal Plane using Adaptive Control Laws Based on Neural Networks and Dynamic Inversion (Q2970896) (← links)
- Adaptive trajectory generation based on real-time estimated parameters for impaired aircraft landing (Q5025861) (← 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)
- An improved NSGA-II based control allocation optimisation for aircraft longitudinal automatic landing system (Q5382588) (← links)
- Robust automatic aircraft lateral beam guidance control using gain-phase margin tester method (Q5931360) (← links)