AEROSPACE TECHNOLOGY JAPAN, THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
Online ISSN : 1884-0477
ISSN-L : 1884-0477
Passenger Aircraft Optimal Trajectory with an Arrival Time Constraint
Yoshikazu MIYAZAWANavinda Kithmal WICKRAMASINGHEAkinori HARADAYuto MIYAMOTO
Author information
JOURNAL FREE ACCESS

2013 Volume 12 Pages 31-38

Details
Abstract
In the future air transportation system, airspace will be efficiently used and each aircraft can optimize its own performance. Due to limited capacity of the airspace like terminal area, however, some sort of adjustment for each aircraft is necessary to maintain separation among multiple aircraft. Fixed arrival time is a basic solution to the problem. This paper studies the effect of arrival time assignment on the performance by assuming that each aircraft generates its own flight plan by minimizing its fuel consumption. Dynamic programming trajectory optimization is used to calculate the optimal flight profile composed of altitude and velocity. The result shows that the arrival time adjustment is efficiently performed in the descent phase, if the required amount of time to be adjusted is not large.
Content from these authors
© 2013 The Japan Society for Aeronautical and Space Sciences
Previous article Next article
feedback
Top