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Missile Target Engagement

version 1.0.0 (52.1 KB) by Arun Suresh
A small test study on guidance of missiles using proportional navigation


Updated 07 Apr 2021

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The proportional navigation guidance law issues acceleration commands, perpendicular to the instantaneous missile-target line of sight, which are proportional to the line-of-sight rate and closing velocity

Cite As

Arun Suresh (2021). Missile Target Engagement (, MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2021a
Compatible with any release
Platform Compatibility
Windows macOS Linux
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