Title :
Missile Acceleration in Proportional Navigation
Author_Institution :
Ministry of Defence Armament Development Authority Tel-Aviv, Israel
fDate :
5/1/1973 12:00:00 AM
Abstract :
In a previous paper, the author obtained conditions for the acceleration of a missile pursuing a maneuvering target according to proportional navigation, to be bounded. This correspondence extends previous work, and new boundaries are obtained for the missile acceleration.
Keywords :
Acceleration; Equations; Missiles; Navigation;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1973.309733
