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Jun 15, 2018 · In order to overcome this problem, a typical solution is to insert a proper midcourse phase inside the missile guidance strategy, through which ...
Abstract: Midcourse phase of a medium-range missile guidance is actually a two point boundary value problem (TPBVP) that is too time-consuming to be ...
Midcourse phase of a medium-range missile guidance is actually a two point boundary value problem (TPBVP) that is too time-consuming to be implemented on an ...
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An optimal midcourse guidance method for dual pulse air-to-air missiles using linear Gauss pseudospectral model predictive control method · Delayed Decision ...
In this paper, we utilize two professional and known sparse kernel machines, the support vector machine (SVM) and the relevance vector machine (RVM), in their ...
An optimal midcourse guidance method for dual pulse air-to-air missiles using linear Gauss pseudospectral model predictive control method · Control problems on ...
Optimal midcourse guidance of an air-to-air missile via SVM and RVM. MR Mortazavi, F Almasganj. Soft Computing 23 (15), 6603-6616, 2019. 7, 2019.
A passive guidance method is used in midcourse guidance stage of long range air-to-air anti-radiation missile, which based on the passive location theory of ...
Optimal intercept trajectories for a boost-sustain-coast medium-range air-to-air missile are synthesized using optimal control theory.
Missing: SVM RVM.
Abstract. The nature of the optimum solution with respect to the timing of interplanetary midcourse guidance maneuvers is investigated.