□ 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
2012-10-01
1987638 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Optimal profile descent with 4-D trajectory
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|Optimal profile descent with 4-D trajectory
IEEE | 2013
|