SATELLITE ATTITUDE CONTROL BY REACTION JET FREQUENCY MODULATION = CONTROLE D'ATTITUDE D'UN SATELLITE PAR MODULATION DE FREQUENCE DU JET A REACTIONBERNUSSOU J.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 52-55; BIBL. 6 REF.Serial Issue

SUR LE CHOIX DE LA FREQUENCE DE MESURE LORS DE LA DETERMINATION DE L'ORIENTATION D'UN SATELLITE ARTIFICIELNOVAK BL.1972; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1972; VOL. 10; NO 6; PP. 859-863; BIBL. 2 REF.Serial Issue

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

OPTIMALE STEUERUNGEN FUER DRALLSTABILISIERTE FLUGKOERPER = COMMANDE OPTIMALE DES ENGINS DE VOL STABILISES PAR ROTATIONLUNDERSTADT R.1973; Z. ANGEW. MATH. MECH.; DTSCH.; DA. 1973; VOL. 53; NO 4; PP. 52-55; BIBL. 3 REF.; (VORTR. WISS. JAHRESTAG. GES. ANGEW. MATH. MECH.; LJUBLJANA; 1972)Conference Paper

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

THE DOUBLE GIMBALLED "DRALLRAD" AND ITS POSSIBLE USE FOR THREE-AXIS-STABILIZATION OF APPLICATION SATELLITESSCHROPL H; REIMERS CJ.1973; J. BRIT. INTERPLANET. SOC.; G.B.; DA. 1973; VOL. 26; NO 2; PP. 106-112Serial Issue

QUELQUES PARAMETRES LIMITES D'UN APPAREIL OPTO-ELECTRONIQUE POUR LA DETERMINATION DE L'ORIENTATION D'UN SPATIONEF PAR RAPPORT AU SOLEILPAVLOV AV; SITKIKOV YU F; PERMYAKOV VD et al.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 2; PP. 340-343; BIBL. 3 REF.Serial Issue

ATTITUDE CONTROL OF A SPINNING SKYLAB = CONTROLE D'ATTITUDE D'UN SKYLAB EN ROTATIONSELTZER SM; SCHWEITZER G; ASNER B JR et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 200-207; BIBL. 9 REF.Serial Issue

USE OF MAGNETOMETERS AND ASYMMETRIC ANTENNA PATTERNS FOR ATTITUDE DETERMINATION = UTILISATION DE MAGNETOMETRES ET DE DIAGRAMMES ASYMETRIQUES D'ANTENNES POUR LA DETERMINATION D'ATTITUDEDELFICO AN; GRAEDEL TE; PRINGLE R JR et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 903-908; BIBL. 2 REF.Serial Issue

ATTITUDE CONTROL OF THE SME SATELLITE: A FLIGHT EXPERIENCESTEWART KD; COWLEY JR; LAWRENCE GM et al.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 507-536; BIBL. 4 REF.Conference Paper

AUTONOMOUS ATTITUDE CONTROLWILLIAMSON RK; MANKE GM; GILLEY GC et al.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 383-396; BIBL. 6 REF.Conference Paper

THE ATTITUDE DETERMINATION AND CONTROL SYSTEM FOR THE SOLAR MESOPHERE EXPLORER SATELLITESTEWART KD.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 234-240; BIBL. 4 REF.Conference Paper

A BASIC ATTITUDE INSTABILITY OF SPACECRAFT WITH IMPERFECT MOMENTUM WHEELS = UNE INSTABILITE D'ATTITUDE FONDAMENTALE D'UN VEHICULE SPATIAL AVEC DES ROUES MOTRICES IMPARFAITESTONKIN SW.1980; AUTOMATICA (OXF.); ISSN 0005-1098; GBR; DA. 1980; VOL. 16; NO 4; PP. 415-418; BIBL. 2 REF.Article

TWO DECADES OF SPACECRAFT ATTITUDE CONTROLROBERSON RE.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-7; 8 P.; BIBL. 30 REF.Conference Paper

ON-BOARD OPTICAL NAVIGATION DATA FROM MARINER 71 = DONNEES DU SYSTEME DE NAVIGATION OPTIQUE A BORD PROVENANT DE MARINER 71DUXBURY TC; ACTON CH JR.1972; NAVIGATION; U.S.A.; DA. 1972; VOL. 19; NO 4; PP. 295-307; BIBL. 5 REF.Serial Issue

SIMULTANEOUS CALIBRATIONS OF VOYAGER CELESTIAL AND INERTIAL ALTITUDE CONTROL SYSTEMS IN FLIGHTJAHANSHAHI MH.1982; IEEE TRANS. AEROSP. ELECTRON. SYST.; ISSN 0018-9251; USA; DA. 1982; VOL. 18; NO 1; PP. 21-28; BIBL. 8 REF.Article

FINE ATTITUDE CONTROL OF AN EARTH OBSERVATION SATELLITE WITH A DISSYMMETRICAL ROTATING SOLAR ARRAYCHRETIEN JP; REBOULET C; RODRIGO P et al.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 121-130; BIBL. 3 REF.Conference Paper

ATTITUDE CONTROL OF GEOSTATIONARY SATELLITES WITH DOUBLE GIMBALLED MOMENTUM WHEELS = COMMANDE D'ATTITUDE DE SATELLITES GEOSTATIONNAIRES DONT LA ROUE GYROSCOPIQUE EST SUSPENDUE PAR UN DOUBLE CORDONSCHULZ G; LANGE T.1981; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1981; AGARD/AG-260; PP. 1.1-1.25; BIBL. 10 REF.Report

DYNAMICS AND CONTROL OF LARGE SPINNING SPACECRAFTJUANG JN; BALAS M.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS - AMERICAN ASTRONAUTICAL SOCIETY ASTRODYNAMICS CONFERENCE/1978/PALO ALTO CA; USA; NEW YORK: AIAA; DA. 1978; 78-1420; 8 P.; BIBL. 11 REF.Conference Paper

SATELLITE ATTITUDE ACQUISITION BY MOMENTUM TRANSFER.BARBA PM; AUBRUN JN.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 10; PP. 1382-1386; BIBL. 1 REF.Article

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

STAR SCANNER ATTITUDE DETERMINATION FOR THE OSO-7 SPACECRAFT = DETERMINATION D'ATTITUDE PAR BALAYAGE D'ETOILES POUR LE VEHICULE SPATIAL OSO-7MACKISON DL; GUTSHALL RL; VOLPE F et al.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 262-267; BIBL. 8 REF.Serial Issue

ISSLEDOVANIE KOSMICHESKOGO PROSTRANSTVA. III. METODY I SISTEMY NAVIGATSII, NAVEDENIYA I UPRAVLENIYA KOSMICHESKIKH LETATEL'NYKH APPARATOV = ETUDE DE L'ESPACE COSMIQUE. TOME 3. METHODES ET SYSTEMES DE NAVIGATION, DU GUIDAGE ET DE COMMANDE DES SPATIONEFSTUVAEV VA.1972; MOSKVA; VINITI; DA. 1972; PP. 1-227; BIBL. DISSEM.; (ITOGI NAUKI TEKH.)Book

PRECISION AUTONOMOUS SATELLITE ATTITUDE CONTROL USING MOMENTUM TRANSFER AND MAGNETIC TORQUINGJUNKINS JL; RAJARAM S; BARACAT WA et al.1982; J. ASTRONAUT. SCI.; ISSN 0021-9142; USA; DA. 1982; VOL. 30; NO 1; PP. 31-48; BIBL. 14 REF.Article

VOYAGER 2 SATURN ENCOUNTER ATTITUDE AND ARTICULATION CONTROL EXPERIENCEHILL M.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 477-505; BIBL. 8 REF.Conference Paper