Naval Postgraduate School
Theses and Dissertations
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A method of increasing the kinematic boundary of air-to-air missiles using an optimal control approach
(Monterey, California. Naval Postgraduate School, 2000-09-01)
Current missile guidance laws are generally based on one of several forms of proportional navigation (PN). While PN laws are robust, analytically tractable, and computationally simple, they are only optimal in a narrow ...
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