Title :
Optimal control application in supersonic aircraft performance
Author_Institution :
University of Michigan, Department of Electrical & Computer Engineering and the Department of Computer, Information & Control Engineering, Ann Arbor, USA
fDate :
7/1/1982 12:00:00 AM
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;
Journal_Title :
Control Theory and Applications, IEE Proceedings D
Conference_Location :
7/1/1982 12:00:00 AM
DOI :
10.1049/ip-d.1982.0023
