Magnetic detumbling of a rigid spacecraft

Journal of Guidance, Control, and Dynamics

Volumn 35, Issue 4, 2012, Pages 1326-1334

  Avanzini, Giulio ^a,c   Giulietti, Fabrizio ^b,d  

^a UNIVERSITY OF SALENTO   (Italy)

^b UNIVERSITY OF BOLOGNA   (Italy)

^c Cittadella della Ricerca   (Italy)

^d Department of Mechanical and Aerospace Engineering ^*  (Italy)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL THEORY; MAGNETISM; MONTE CARLO METHODS;

ASYMPTOTIC CONVERGENCE; INITIAL CONDITIONS; MATHEMATICAL PROOF; MONTE CARLO APPROACH; REASONABLE VALUE; RIGID SPACECRAFT; TIME-VARYING MAGNETIC FIELDS; TUMBLING CONDITION;

MAGNETIC ACTUATORS;

EID: 84867089999     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.53074     Document Type: Article

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