DocumentCode
676993
Title
A method to design a tie-point-based Optimized Profile Descent (OPD) solution
Author
Grabow, Christian
Author_Institution
Boeing Research & Technology Europe (BR&TE), USA
fYear
2013
fDate
5-10 Oct. 2013
Firstpage
1
Lastpage
15
Abstract
▪ Tie-point concept can enable a high number of OPDs with current ground and aircraft equipage ▪ A method to optimize the tie-point concept design (i.e., tie-point distance, speed tables and altitude windows) was presented ▪ The design method is based on fast-time simulations
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2013 IEEE/AIAA 32nd
Conference_Location
East Syracuse, NY, USA
ISSN
2155-7195
Print_ISBN
978-1-4799-1536-1
Type
conf
DOI
10.1109/DASC.2013.6719598
Filename
6719598
Link To Document