DocumentCode
791686
Title
Quasi-optimum control for minimum-time rendezvous
Author
Friedland, B. ; Cohen, V.
Author_Institution
Aerospace Research Center, General Precision, Inc., Little Falls, NJ, USA
Volume
11
Issue
3
fYear
1966
fDate
7/1/1966 12:00:00 AM
Firstpage
525
Lastpage
528
Abstract
A quasi-optimum control law for minimum-time, bounded acceleration rendezvous in a plane is obtained. By ignoring the tangential velocity, a simplified problem is obtained for which there is a well-known solution. The tangential velocity is then accounted for, approximately, by use of the quasi-optimum control technique described by Friedland.1 Simulated trajectories show that the quasi-optimum control law gives excellent results.
Keywords
Optimal control; Rendezvous methods; Acceleration; Control systems; Control theory; Costs; Differential equations; Feedback control; Real time systems; Riccati equations; Symmetric matrices; Velocity control;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1966.1098343
Filename
1098343
Link To Document