M. Guelman
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.
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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.
Key concepts: Acceleration, Proportional navigation, Missile, Bounded function, Missile guidance, Work (physics), Control theory (sociology), Computer science