Abstract The elements for various types of attitude control systems used in a number of small spacecraft are considered. An approach for assessment of such system effectiveness based on design requirements for spacecraft purpose and restriction in accuracy, mass and energy is proposed.
An approach to forming the design performance of the attitude control system for small spacecraft
Russian Aeronautics (Iz VUZ) ; 58 , 4 ; 376-382
2015-10-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
An approach to forming the design performance of the attitude control system for small spacecraft
Online Contents | 2015
|Attitude determination and control for small spacecraft
IET Digital Library Archive | 1996
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