Open AccessStrategy for the development of the stabilization system ICRC spacecraft in various fields
Author(s) -
В. Л. Бычков,
V. G. Cherkashin
Publication year - 2021
Publication title -
nacionalʹnaâ bezopasnostʹ i strategičeskoe planirovanie
Language(s) - English
Resource type - Journals
ISSN - 2307-1400
DOI - 10.37468/2307-1400-2021-1-25-33
Subject(s) - spacecraft , relative motion , center of mass (relativistic) , orientation (vector space) , motion (physics) , aerospace engineering , angular velocity , center (category theory) , circular motion , physics , control (management) , control theory (sociology) , computer science , engineering , mathematics , classical mechanics , artificial intelligence , geometry , chemistry , energy–momentum relation , crystallography
Control of spacecraft motion relative to its center of mass, depending on their specific purpose and intended program of application (for example, reconnaissance and output of target designation (CA)), is generally reduced to provision of specified angular motion of spacecraft relative to its center of mass and its angular orientation with specified accuracy.