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AERODYNAMIC BEHAVIOR OF THE VIKING ENTRY VEHICLE: GROUND TEST AND FLIGHT RESULTSKIRK DB; INTRIERI PF; SEIFF A et al.1978; J. SPACECR. ROCK.; USA; DA. 1978; VOL. 15; NO 4; PP. 208-212; BIBL. 12 REF.Article

PROGRESS IN MODELLING AND CONTROL OF FLEXIBLE SPACECRAFTJOHNSON TL.1983; JOURNAL OF THE FRANKLIN INSTITUTE; ISSN 0016-0032; USA; DA. 1983; VOL. 315; NO 5-6; PP. 495-530; BIBL. 80 REF.Article

THERMAL CONVECTION IN AN ENCLOSURE DUE TO VIBRATIONS ABOARD SPACECRAFTKAMOTANI Y; PRASAD A; OSTRACH S et al.1981; AIAA J.; ISSN 0001-1452; USA; DA. 1981; VOL. 19; NO 4; PP. 511-516; BIBL. 10 REF.Article

THE CONTROL OF SPACECRAFT VIBRATIONS USING MULTIVARIABLE OUTPUT FEEDBACKCANAVIN JR.1978; AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS - AMERICAN ASTRONAUTICAL SOCIETY ASTRODYNAMICS CONFERENCE/1978/PALO ALTO CA; USA; NEW YORK: AIAA; DA. 1978; 78-1419; 11 P.; BIBL. 12 REF.Conference Paper

DYNAMICS OF INTERSTAGE SEPARATION FOR A DMSP SPACECRAFT: HYPOTHESIS TESTING OF A FLIGHT ANOMALYMAK PH; MUELHAUPT TJ; LOPEZ JM et al.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 457-475Conference 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

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

FAST THREE-AXIS ATTITUDE DETERMINATION USING VECTOR OBSERVATIONS AND INVERSE ITERATIONTIETZE JL.1982; J. ASTRONAUT. SCI.; ISSN 0021-9142; USA; DA. 1982; VOL. 30; NO 2; PP. 171-179; BIBL. 5 REF.Article

SMM ATTITUDE CONTROL RECOVERYHOFFMAN HC; DONOHUE JH; FLATLEY TW et al.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 84-90Conference Paper

NUCLEAR WASTE DISPOSAL IN SPACE: IMPLICATIONS OF ADVANCED SPACE TRANSPORTATIONSALKELD R; BEICHEL R.1980; ACTA ASTRONAUT.; ISSN 0094-5765; USA; DA. 1980; VOL. 7; NO 12; PP. 1373-1387; BIBL. 18 REF.Article

TRENDS IN THE AUTOMATION OF PLANETARY SPACECRAFTBIRD TH; SHEAHAN RR.1979; ASTRONAUT. AND AERONAUT.; USA; DA. 1979; VOL. 17; NO 5; PP. 32-35Article

CARACTERISATION DES AEROSOLS BACTERIENS DANS DES ENCEINTES HABITEES PAR L'HOMME PRESENTANT DES ATMOSPHERES DE VAISSEAU SPATIALZALOGUEV SN; VIKTOROV AN; POZHARSKIJ GO et al.1978; KOSM. BIOL. AVIAKOSM. MED.; SUN; DA. 1978; VOL. 12; NO 5; PP. 72-75; ABS. ENG; BIBL. 10 REF.Article

EFFECTS OF FLEXIBILITY ON AGS PERFORMANCESHELTON HL; CUNNINGHAM DC; SELTZER SM et al.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 3-17Conference Paper

INERTIAL UPPER STAGE (IUS) MULTI-MISSION ADAPTILITY VIA GAMMA GUIDANCE SOFTWARE MENU TABLESHARDTLA JW; SCHULTZ LA.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 213-227; BIBL. 1 REF.Conference Paper

SIMULATION OF ATMOSPHERIC TURBULENT GUSTS AND GUSTS GRADIENTSTATOM FB; SMITH SR; FICHTL GH et al.1982; J. AIRCR.; ISSN 0021-8669; USA; DA. 1982; VOL. 19; NO 4; PP. 264-271; BIBL. 20 REF.Article

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

SPIN-CONTROLLED MANEUVER STRATEGIES USING UNBALANCED PRECESSIONSKECHICHIAN JA.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 91-120; BIBL. 6 REF.Conference Paper

AUTONOMOUS ATTITUDE DETERMINATION FROM STAR DATA FOR A DUAL-SPIN PLANETARY SPACECRAFT = DETERMINATION AUTONOME D'ATTITUDE A PARTIR DE DONNEES STELLAIRES POUR UN ENGIN SPATIAL PLANETAIRE A DOUBLE PLAN DE ROTATIONWONG EC; LAI JY.1981; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1981; AGARD/AG-260; PP. 3.1-3.15; BIBL. 11 REF.Report

SLEWING MANEUVERS OF GYROSTAT SPACECRAFTCHEN J; KANE TR.1980; J. ASTRONAUT. SCI.; ISSN 0021-9142; USA; DA. 1980; VOL. 28; NO 3; PP. 267-281Article

APPLICATION OF KALMAN FILTERING TO SPACECRAFT RANGE RESIDUAL PREDICTION.MADRID GA; BIERMAN GJ.1978; I.E.E.E. TRANS. AUTOMAT. CONTROL; USA; DA. 1978; VOL. 23; NO 3; PP. 430-433; BIBL. 7 REF.Article

ECUACIONES DE GUIADO DE FIN DE COMBUSTION (TIERRA ESFERICA) = EQUATIONS DE GUIDAGE EN FIN DE COMBUSTION (TERRE SPHERIQUE)ELICES CONCHA T.1980; I.N.T.A. CO. N.I.E., INFORM. AEROESPACIAL; ESP; DA. 1980; NO 19; PP. 5-10Article

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

PREVALENCE OF FUNGI DURING SKYLAB MISSIONS.BROCKETT RM; FERGUSON JK; HENNEY MR et al.1978; APPL. ENVIRONMENT. MICROBIOL.; USA; DA. 1978; VOL. 36; NO 2; PP. 243-246; BIBL. 8 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

AMBIGUITIES IN SPACEBORNE SYNTHETIC APERTURE RADAR SYSTEMSLI FK; JOHNSON WTK.1983; IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS; ISSN 0018-9251; USA; DA. 1983; VOL. 19; NO 3; PP. 389-397; BIBL. 11 REF.Article

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