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In the work "Optimization methodology of hierarchical control of orbit constellations" a new approach is proposed to the research of hierarchical optimization problem of large control systems. The unique methods are developed which allow determining the laws of spacecraft optimal control during the different flight stages without the use of complicated calculation procedures of boundary tasks solution. The development of hierarchical principles of optimization is one of the tendencies for methodology improvement of research of control operations in different areas of science and technology. The proposed methodological approach can be widely used in the fields of space navigation, aviation, machine building, monitoring of near earth space, mathematical modelling, optimal control.
A propos de l'auteur
Nikolay Leonidovich Sokolov is candidate of science (Engineering), expert in optimal control. Author of 80 works and 15 patents for spacecraft control methods. He held the position of flight director of ten satellites. At present Nikolay Sokolov is Deputy Head of the Mission Control Centre of the Central Research Institute of Machine Building.
