DocumentCode
3558005
Title
Optimal control application in supersonic aircraft performance
Author
Lin, Ching-Fang
Author_Institution
University of Michigan, Department of Electrical & Computer Engineering and the Department of Computer, Information & Control Engineering, Ann Arbor, USA
Volume
129
Issue
4
fYear
1982
fDate
7/1/1982 12:00:00 AM
Firstpage
113
Lastpage
117
Abstract
Optimal control theory is used in the analysis of the three-dimensional turning performance of supersonic aircraft to generate real-time online optimal trajectories.
Keywords
aerospace control; aircraft; optimal control; optimal control; real-time online optimal trajectories; supersonic aircraft; three-dimensional turning performance;
fLanguage
English
Journal_Title
Control Theory and Applications, IEE Proceedings D
Publisher
iet
Conference_Location
7/1/1982 12:00:00 AM
ISSN
0143-7054
Type
jour
DOI
10.1049/ip-d.1982.0023
Filename
4642116
Link To Document