DocumentCode
2547747
Title
Fixed RTA fuel optimal profile descent based on analysis of trajectory performance bound
Author
Sang Gyun Park ; Clarke, J.B.
fYear
2012
fDate
14-18 Oct. 2012
Firstpage
1
Lastpage
27
Abstract
A collection of slides from the author´s conference presentation is given. The following topics are discussed: TPA framework 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; and the suboptimal trajectory shows the similar performance comparing to real optimal trajectory.
Keywords
aircraft control; design engineering; fuel; suboptimal control; trajectory control; vehicle dynamics; RTA fuel optimal profile; TPA framework; aircraft dynamics; fixed RTA suboptimal trajectory generation method; optimal control; real optimal trajectory; trajectory performance analyzer; trajectory performance bound; trajectory structure design;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference (DASC), 2012 IEEE/AIAA 31st
Conference_Location
Williamsburg, VA
ISSN
2155-7195
Print_ISBN
978-1-4673-1699-6
Type
conf
DOI
10.1109/DASC.2012.6382992
Filename
6382992
Link To Document