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
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
Conference_Titel :
Digital Avionics Systems Conference (DASC), 2013 IEEE/AIAA 32nd
Conference_Location :
East Syracuse, NY, USA
Print_ISBN :
978-1-4799-1536-1
DOI :
10.1109/DASC.2013.6719598
