EQUILIBRIUM ATTITUDE TRANSITIONS OF A THREE-ROTOR GYROSTAT IN A CIRCULAR ORBIT = TRANSITION D'ATTITUDE D'EQUILIBRE POUR UN GYROSTAT A TROIS ROTORS SUR UNE ORBITE CIRCULAIREANCHEV AA.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 4; PP. 467-472; BIBL. 5 REF.Serial Issue

ERREURS D'UN SYSTEME DE STABILISATION PAR GRAVITATION D'UN SATELLITE AVEC UN GYROAMORTISSEMENTBELYAEVA GM.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 2; PP. 330-332; BIBL. 2 REF.Serial Issue

GRAVITY-GRADIENT STABILIZATION OF SYNCHRONOUS ORBITING SATELLITES-ADDITIONAL CONSIDERATIONS OF ATTITUDE STABILITY = STABILISATION PAR GRADIENT DE GRAVITE DE SATELLITES SYNCHRONES. CONSIDERATIONS SUPPLEMENTAIRES SUR LA STABILITE D'ATTITUDEBAINUM PM.1973; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1973; VOL. 26; NO 6; PP. 343-347; BIBL. 5 REF.Serial Issue

THREE-DIMENSIONAL MOTION OF A LARGE FLEXIBLE SATELLITEBUDYNAS R; POLI C.1972; AUTOMATICA; G.B.; DA. 1972; VOL. 8; NO 3; PP. 275-286; ABS. FR. ALLEM. RUSSE; BIBL. 24 REF.Serial Issue

CONTRIBUTION A L'ETUDE DE LA STABILITE D'ATTITUDE DES SATELLITES ARTIFICIELS PASSIFS PARCOURANT UNE TRAJECTOIRE ELLIPTIQUEBONTHOUX CG.1973; AO-CNRS-8203; FR.; DA. 1973; PP. 1-188; BIBL. 8 P. 1/2; (THESE DOCT. SCI. PHYS.; PARIS VI)Thesis

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