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.
Missile Acceleration in Proportional Navigation
IEEE Transactions on Aerospace and Electronic Systems ; AES-9 , 3 ; 462-463
01.05.1973
297365 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch