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Missile Acceleration in Proportional Navigation

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1 Author(s)
Guelman, M. ; Ministry of Defence Armament Development Authority Tel-Aviv, Israel

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.

Published in:

Aerospace and Electronic Systems, IEEE Transactions on  (Volume:AES-9 ,  Issue: 3 )