Airplane trajectory control at the stage of rendezvous with maneuvering object algorithms synthesis

It´s considered the capability of developed before simplified modification of direct method of boundary trajectory optimizational tasks with the fixed edges conditions solution application for formation of near-optimal trajectories in tasks with mobile right end. The possibility and expediency of permissible controls class expansion is investigated from the standpoint of labor input of solution obtaining and effectiveness of this solution. Examples of particular quasi-optimal solutions are discussed. The applicability of the developed algorithms both for mathematical modeling on fixed computers and for realization in onboard pilot´s control actions during maneuvering support system (system of real time) is evaluated