Synthesis of Algorithm to Change Guidance Law for Air-to-Air Missiles Intercept Separating Targets
DOI:
https://doi.org/10.3849/aimt.01836Keywords:
algorithm of choosing optimal guidance laws, separating target, supermaneuverable target, optimal proportional pre-emptive navigation lawAbstract
This paper presents the results of summarizing the algorithm of target selection and
changing guidance law applied for medium and long-range air-to-air intercept missiles
to ensure the ability to detect and distinguish the group-separating target, which in turn
improving the efficiency in tracking and terminating the selected targets. The proposed
algorithm reduces the miss distance to a minimal value while ensuring two primary
requirements, including distinguishing each target in the group by Doppler frequency
and identifying the flight direction of the target to track and destroy.
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