Two NASA goals are to enhance airport safety and to improve capacity in all weather conditions. This paper contributes to these goals by examining speed guidance profiles to aid a pilot in decelerating along the runway to an exit. A speed profile essentially tells the pilot what the airplane's speed should be as a function of where the airplane is on the runway. While it is important to get off the runway as soon as possible (when striving to minimize runway occupancy time), the deceleration along a speed profile should be constrained by passenger comfort. Several speed profiles are examined with respect to their maximum decelerations and times to reach exit speed. One profile varies speed linearly with distance; another has constant decele...
Presently Distance Based Separation (DBS) rules are applied during final approach. As these rules re...
Amsterdam Schiphol Airport currently uses a Continuous Descent Approach during night time operations...
This research addresses the problem of the definition and calculation of the landing point-of-no-ret...
This report defines the initial requirements for designing a research high-speed rollout and turnoff...
The decelerate-accelerate-takeoff maneuver in transport category airplanes has been discussed. Mathe...
The decelerate-accelerate-takeoff maneuver in transport category airplanes has been discussed. Mathe...
Landing delays are currently a problem at major air carrier airports and many forecasters agree that...
The take-off distances over a 35-foot obstacle have been determined for a supersonic transport confi...
This study develops a lateral deviation based framework for identifying potential veer off risks at...
A study developed for the TCV B-737, designed to apply existing navigation aids plus magnetic leader...
PURPOSES: Previous Speed Profile reflects the patterns of speeds in sections of tangents to curves i...
Over the past thirty years, the civil aeronautical community has actively pursued research to enable...
Two of the major projects in ATM development, SESAR and NextGen, both fore- cast the use of 4D traje...
This report examines a rollout and turnoff (ROTO) system for reducing the runway occupancy time for ...
The precise guidance and control of taxiing aircraft based on four-dimensional trajectories (4DTs) h...
Presently Distance Based Separation (DBS) rules are applied during final approach. As these rules re...
Amsterdam Schiphol Airport currently uses a Continuous Descent Approach during night time operations...
This research addresses the problem of the definition and calculation of the landing point-of-no-ret...
This report defines the initial requirements for designing a research high-speed rollout and turnoff...
The decelerate-accelerate-takeoff maneuver in transport category airplanes has been discussed. Mathe...
The decelerate-accelerate-takeoff maneuver in transport category airplanes has been discussed. Mathe...
Landing delays are currently a problem at major air carrier airports and many forecasters agree that...
The take-off distances over a 35-foot obstacle have been determined for a supersonic transport confi...
This study develops a lateral deviation based framework for identifying potential veer off risks at...
A study developed for the TCV B-737, designed to apply existing navigation aids plus magnetic leader...
PURPOSES: Previous Speed Profile reflects the patterns of speeds in sections of tangents to curves i...
Over the past thirty years, the civil aeronautical community has actively pursued research to enable...
Two of the major projects in ATM development, SESAR and NextGen, both fore- cast the use of 4D traje...
This report examines a rollout and turnoff (ROTO) system for reducing the runway occupancy time for ...
The precise guidance and control of taxiing aircraft based on four-dimensional trajectories (4DTs) h...
Presently Distance Based Separation (DBS) rules are applied during final approach. As these rules re...
Amsterdam Schiphol Airport currently uses a Continuous Descent Approach during night time operations...
This research addresses the problem of the definition and calculation of the landing point-of-no-ret...