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AN APPROXIMATE SEMI-ANALYTICAL SOLUTION FOR ORBIT- AND ATTITUDE MANEUVERS OF SPIN-STABILIZED SATELLITES.

Author
ECKSTEIN MC
DFVLR, OBERPFAFFENHOFEN, F.R.G.
Source
CELEST. MECH.; NETHERL.; DA. 1976; VOL. 14; NO 3; PP. 307-320; BIBL. 7 REF.
Document type
Article
Language
English
Keyword (fr)
MECANIQUE CELESTE SATELLITE ARTIFICIEL EQUATION MOUVEMENT ASTRONOMIE
Keyword (en)
CELESTIAL MECHANICS ARTIFICIAL SATELLITE EQUATION OF MOTION ASTRONOMY
Keyword (es)
ASTRONOMIA
Classification
Pascal
001 Exact sciences and technology / 001E Earth, ocean, space / 001E03 Astronomy

Discipline
Astronomy
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
PASCAL7730194351

Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS

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