DocumentCode
1343137
Title
Optimal guidance laws with uncertain time-of-flight
Author
Rusnak, Ilan
Author_Institution
RAFAEL, Haifa
Volume
36
Issue
2
fYear
2000
fDate
4/1/2000 12:00:00 AM
Firstpage
721
Lastpage
725
Abstract
The existing optimal guidance laws assume that the time-to-go is known exactly. The time-to-go is usually estimated and thus is a random variable. The issue of optimal guidance with uncertain time-to-go is dealt with here. A problem of the control of linear discrete systems with unknown time-to-go is formulated and solved. The solution is applied to derive guidance laws. The solution depends on the probability density function of the time-of-flight. This guidance law has the structure of a rendezvous guidance law where the guidance gains are time-dependent and depend on the distribution of the time-to-go. Examples that demonstrate these dependencies are presented
Keywords
discrete systems; linear systems; missile guidance; optimal control; probability; PDF; linear discrete systems; missiles; optimal guidance laws; probability density function; rendezvous guidance law; uncertain time-of-flight; Continuous time systems; Cost function; Equations; Missiles; Navigation; Optimal control; Probability density function; Random variables; Regulators; Uncertainty;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.845272
Filename
845272
Link To Document