The influence of several parameters on the time required to fly a nominal profile descent of a B-737 from an entry fix to a metering fix 75 n.mi. away was studied. The ground distance for the constant speed segment was adjusted in each case so that the aircraft would always arrive at the metering fix position at the completion of the five segments of the profile descent. The influence of eight parameters on the same nominal profile descent is outlined, but the method used for the off nominal cases was changed. The time calculated for the constant speed segment in the nominal case is used for all off nominal cases. This method allows the aircraft to arrive at the metering fix before or after the profile descent is complete. It is shown that ...
An analytical formula for solving the speed profile that accrues minimum cost during an aircraft des...
The ability to meet a controlled time of arrival during a continuous descent operation will enable e...
A study was conducted to determine the effect of head-wind profiles and mean head-wind velocities on...
Concepts to save fuel while preserving airport capacity by combining time based metering with profil...
This paper compares fuel consumption of descent trajectories from cruise altitude to meter fix when ...
This paper compares fuel consumption of alternative descent trajectories from cruise altitude to met...
A simple flight management descent algorithm designed to improve the accuracy of delivering an airpl...
A simplified flight management descent algorithm was developed and programmed on a small programmabl...
One of the goals of NextGen is to enable frequent use of Optimized Profile Descents (OPD) for aircra...
Rising fuel costs combined with other economic pressures have resulted in industry requirements for ...
To enable arriving aircraft to fly optimized descents computed by the flight management system (FMS)...
To enable arriving aircraft to fly optimized de-scents computed by the flight management system (FMS...
A study was conducted to evaluate the benefits of an approach technique which utilized constant grou...
The rapidly increasing costs of flight operations and the requirement for increased fuel conservatio...
To enable arriving aircraft to fly optimized descents computed by the flight management system (FMS)...
An analytical formula for solving the speed profile that accrues minimum cost during an aircraft des...
The ability to meet a controlled time of arrival during a continuous descent operation will enable e...
A study was conducted to determine the effect of head-wind profiles and mean head-wind velocities on...
Concepts to save fuel while preserving airport capacity by combining time based metering with profil...
This paper compares fuel consumption of descent trajectories from cruise altitude to meter fix when ...
This paper compares fuel consumption of alternative descent trajectories from cruise altitude to met...
A simple flight management descent algorithm designed to improve the accuracy of delivering an airpl...
A simplified flight management descent algorithm was developed and programmed on a small programmabl...
One of the goals of NextGen is to enable frequent use of Optimized Profile Descents (OPD) for aircra...
Rising fuel costs combined with other economic pressures have resulted in industry requirements for ...
To enable arriving aircraft to fly optimized descents computed by the flight management system (FMS)...
To enable arriving aircraft to fly optimized de-scents computed by the flight management system (FMS...
A study was conducted to evaluate the benefits of an approach technique which utilized constant grou...
The rapidly increasing costs of flight operations and the requirement for increased fuel conservatio...
To enable arriving aircraft to fly optimized descents computed by the flight management system (FMS)...
An analytical formula for solving the speed profile that accrues minimum cost during an aircraft des...
The ability to meet a controlled time of arrival during a continuous descent operation will enable e...
A study was conducted to determine the effect of head-wind profiles and mean head-wind velocities on...