Multicriteria Optimization Based on Desired Trajectory Form and Multiprogram Point-to-Point Control

The article considers a promising technology of multicriteria optimization based on multiprogram point-to-point control for forming trajectories ensuring efficient target hit, using the problem of spatial missile guidance as an example. In order to significantly reduce the unknown parameter search space dimension, instead of parametrising the control itself we transition to a search space for parameters of a certain desired reference trajectory form. We form the solution set (state and control vectors as functions of time, plus optimisation criteria values) based on "gravitating" towards reference trajectories and select the most preferable solution

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