Title :
Comments on "Predictive guidance for interceptors with time lag in acceleration"
Author_Institution :
Raytheon Company, Bedford, MA, USA
fDate :
6/1/1981 12:00:00 AM
Abstract :
Previous solutions related to those in the above paper are pointed out, and some interpretations of the results are given in terms of "zero-effort miss."
Keywords :
Missile guidance; Acceleration; Control systems; Error correction; History; Missiles; Predictive models; Riccati equations; Terminology; Velocity control; Vocabulary;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1981.1102676
