The Formation of the Structure of the Trajectory Control of Flying Vehicle and Multi-Criteria Optimization of its Parameters

The problem of formation structure of trajectory control of the flying vehicle at setting the dynamics by a simultaneous differential equations of motion with direction to the set point of destination and ensuring the required speed of the flying vehicle during the flight and condition of vertical output to the destination is discussed. The structural scheme of directing of flying vehicle which control parameters are the coefficients of the proportional-integral-differential (PID)-controller and the external soft impact on the vertical angle direction of the flying vehicle is studied. Two-stage algorithm of formation of structure of trajectory control with multivariate testing of the desired trajectory of the flying vehicle on the given vector of the requirements in the first stage and multi-criteria optimization of the parameters of the structure of the trajectory control based on ideal point method and network gradient optimization at the second stage is developed. The procedure of formation of distant boundary of the applicability scope of the flying vehicle for various external software impacts with the investigation of direction quality is accomplished.

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