Title :
Missile guidance with constrained intercept body angle
Author :
Rusnak, Ilan ; Weiss, Haim ; Eliav, Rei ; Shima, Tal
Author_Institution :
RAFAEL, Haifa, Israel
Abstract :
A linear quadratic based missile guidance law is presented that imposes a predetermined terminal body angle. Solutions are provided for arbitrary order autopilot dynamics, with explicit analytical expressions given for first-order and zero-lag dynamics. Performance is demonstrated through simulation in a planar interception scenario.
Keywords :
missile guidance; arbitrary order autopilot dynamics; constrained intercept body angle; explicit analytical expressions; first-order dynamics; linear quadratic based missile guidance law; missile guidance; planar interception scenario; terminal body angle; zero-lag dynamics; Acceleration; Aerodynamics; Equations; Geometry; Mathematical model; Missiles; Navigation;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.2014.120100
