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 :
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