Abstract. This paper presents a random calculus model for guidance precision,
and evaluation of target hit and target kill probabilities, in
the case of close range-homing missiles. Due to their non-stationary
character, the guidance equations have been integrated by canonical separation
and the results have been analyzed by comparison for various
tactical situations. Observations about the influence of various parameters on
missile performance have been formulated. The novelty of the paper
resides in application of the theoretical method, from random functions
theory, to solve the technical problem of missile guided-flight modeling,
for which we obtained some interesting and useful results.
Related topics:
guided weapons, firepower and protection
View first page of "Chelaru: Mathematical Calculation Model for Guidance Precision, Target Hit, and Target Kill Probabilities, in the Case of Close Range-Homing Missiles"
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