Attitude determination and control for centrifugal tether deployment on the ESTCube-1 nanosatellite
نویسندگان
چکیده
منابع مشابه
Design of MEMS Based Attitude Determination and Control System for Nanosatellite
-One of the latest manifestations of miniaturization in space applications is the development of standardized nanosatellite. Recent achievements and future trends of Micro-Electro-Mechanical Systems (MEMS) technology have indicated that microtechnology is the critical technologies of future space programs. Enabling technologies for demanding applications will surely make use of MEMS based compo...
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This guideline provides a procedure which specifies and documents consistent, useful, and welldefined coordinate system (or frame) definitions for spacecraft attitude control design and analysis. Several example coordinate frames and transformations are presented to show how these definitions are used to address various Attitude Control System (ACS) design issues. Past experience has shown the ...
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ژورنال
عنوان ژورنال: Proceedings of the Estonian Academy of Sciences
سال: 2014
ISSN: 1736-6046
DOI: 10.3176/proc.2014.2s.05