NASA Technical Reports Server (NASA) · 2002 · 72 citations · 1 references
Open access
EngineeringAerospace EngineeringSystems EngineeringAircraft DesignFlight DynamicsFlight MechanicsAircraft ControlAircraft PerformanceFlight Management SystemsFlight PerformanceFlight SimulationControl Law DesignFlight Path ControlMinimum DistancePrecision Approach ControlPrecision Speed ControlWorkloadWorkload Assessment
This document describes a speed control law for precision in-trail airborne self-spacing during final approach. This control law was designed to provide an operationally viable means to obtain a desired runway threshold crossing time or minimum distance, one aircraft relative to another. The control law compensates for dissimilar final approach speeds between aircraft pairs and provides guidance for a stable final approach. This algorithm has been extensively tested in Monte Carlo simulation and has been evaluated in piloted simulation, with preliminary results indicating acceptability from operational and workload standpoints.
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