Capture Region Analysis for Missile Guidance with Field-of-view Constraint against Moving Target
نویسندگان
چکیده
A capture region for missile guidance laws under field-of-view constraint is analyzed. To make a missile intercept a non-maneuvering target, physical constraints including seeker`s field-of-view and acceleration limit should be considered, because these constraints may restrict maneuver of the interceptor. The characteristics of look-angle constraint guidance laws is studied, and feasible trajectory envelope and achievable impact angle set are derived using deviated pursuit trajectory. To validate the analysis of the capture region, numerical simulation is carried out.
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