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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

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

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

A DOUBLE GIMBALLED MOMENTUM WHEEL FOR 3-AXIS ATTITUDE CONTROLAUER W.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 51-61; BIBL. 12 REF.Conference Paper

IRAS ATTITUDE CONTROL PRINCIPLES AND VERIFICATIONTEULE FJP; VAN DOORN RM.1980; J.A; ISSN 0377-2055; BEL; DA. 1980; VOL. 21; NO 4; PP. 170-176; BIBL. 5 REF.Article

ATTITUDE CONTROL OF A FLEXIBLE SATELLITE IN NOISY ENVIRONMENT = COMMANDE DE L'ORIENTATION D'UN SATELLITE MOBILE LORSQUE LES MESURES DE L'ORIENTATION SONT ENTACHEES DE BRUITFENTON J; HORTON DNL; GILL KF et al.1979; PROC. I.E.E.; ISSN 0020-3270; GBR; DA. 1979; VOL. 126; NO 12; PP. 1307-1310; BIBL. 10 REF.Article

EFFECTS OF STRUCTURAL FLEXIBILITY ON A REACTION JET SATELLITE ATTITUDE CONTROL SYSTEM.MALICH G.1975; U.T.I.A.S. TECH. NOTE; CANADA; DA. 1975; NO 199; PP. (28P.); H.T. 40; BIBL. 10 REF.Article

DEVELOPMENT OF THE GALILEO ATTITUDE AND ARTICULATION CONTROL SUBSYSTEM FLIGHT SOFTWAREKRASNER SM.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 251-267; BIBL. 8 REF.Conference Paper

ACTIVE CONTROL OF DYNAMICS TRANSFER FUNCTIONS FOR A FLEXIBLE SPACECRAFTGARG SC.1979; UTIAS REP.; ISSN 0082-5255; CAN; DA. 1979; VOL. 239; 45 P.; H.T. 32; BIBL. 19 REF.Serial Issue

TWO LEVEL ATTITUDE CONTROL FOR A TELEVISION AND BROADCASTING SATELLITE.BECKER K.1977; AUTOMATICA; G.B.; DA. 1977; VOL. 13; NO 6; PP. 595-604; BIBL. 6 REF.Article

ATTITUDE CAPTURE FOR THE GEODYNAMICS EXPERIMENTAL OCEAN SATELLITE (GEOS)-3.LERNER GM; CORIELL KP.1976; ADV. ASTRONAUT. SCI.; U.S.A.; DA. 1976; VOL. 33; PP. 27-52; BIBL. 7 REF.Article

SATELLITE LIBRATIONAL DAMPING USING A QUASI-FEEDBACK SOLAR CONTROLLERKUMAR K.1982; IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS; ISSN 0018-9251; USA; DA. 1982; VOL. 18; NO 5; PP. 591-597; BIBL. 12 REF.Article

A MICROCOMPUTER BASED SYSTEM FOR ON-BOARD ATTITUDE CONTROL APPLICATIONSGUNZENHAUSER R; WLAKA M; ZAGO HD et al.1979; J. BRIT. INTERPLANET. SOC.; GBR; DA. 1979; VOL. 32; NO 1; PP. 15-23; BIBL. 2 REF.Article

PRELIMINARY TEST RESULTS ON A LASER SYSTEM FOR MEASUREMENT OF ROCKET ATTITUDE DURING FLIGHT TESTPELL KM; NYDAHL JE; BROWN D et al.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS AEROSPACE SCIENCES MEETING. 16/1978/HUNTSVILLE AL; USA; NEW YORK: AIAA; DA. 1978; 78-17; 7 P.; BIBL. 4 REF.Conference Paper

SIMULTANEOUS IN-FLIGHT CALIBRATIONS OF THE GALILEO SCIENCE PLATFORM AND ATTITUDE CONTROL SUBSYSTEMSLAI JY; HAYATI SA.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 500-512; BIBL. 11 REF.Conference Paper

A NUCLEAR SAFING CONTROLLER DESIGN FOR A PRECISION POINTING THREE-AXIS STABILIZED SPACECRAFTBASUTHAKUR S.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 230-233; BIBL. 1 REF.Conference Paper

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