Open AccessКОМБІНОВАНЕ КЕРУВАННЯ КОСМІЧНИМ СТУПЕНЕМ РАКЕТИ-НОСІЯ
Author(s) -
Ю. Д. Шептун
Publication year - 2018
Publication title -
vìsnik dnìpropetrovsʹkogo unìversitetu. serìâ: raketno-kosmìčna tehnìka
Language(s) - English
Resource type - Journals
ISSN - 2409-4056
DOI - 10.15421/451825
Subject(s) - control theory (sociology) , minification , missile , computer science , aerospace engineering , engineering , mathematics , control (management) , mathematical optimization , artificial intelligence
The processes of working out the perturbations of the movement parameters of the LV stages are characterized by features that are not currently taken into account in the algorithms for zeroing perturbations by missile control systems. The article contains proposals on minimization of fuel consumption for zeroing the perturbations of rocket motion parameters.