□ TPA frame work for obtaining trajectory performance bound of individual aircraft is proposed □ Fixed RTA suboptimal trajectory generation method is proposed □ Trajectory structure is designed by analysis of real optimal trajectory □ The suboptimal trajectory shows the similar performance comparing to real optimal trajectory
Fixed RTA fuel optimal profile descent based on analysis of trajectory performance bound
01.10.2012
1987638 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch