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Published in 2018 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2018.05.018
Abstract: Abstract In this paper, a new optimal guidance law with terminal constraints on miss distance and intercept angle is proposed for a missile with time-varying velocity against a maneuvering target. The proposed optimal guidance law…
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Keywords:
tangent function;
intercept angle;
hyperbolic tangent;
guidance law ... See more keywords