STRAPPED DOWN INERTIAL NAVIGATION SYSTEMSCOLLINSON RPG.1973; J. NAVIG.; G.B.; DA. 1973; VOL. 26; NO 3; PP. 341-351; BIBL. 1 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

STRAP-DOWN INERTIAL GUIDANCE SYSTEMS STUDYBALDASSINI FONTANA R.1973; REV. SCI. TECH. C.E.C.L.E.S./C.E.R.S.; FR.; DA. 1973; VOL. 5; NO 1; PP. 35-57; ABS. FR. ALLEMSerial Issue

FORCES ELECTROSTATIQUES PARASITES SUR UNE MASSE D'EPREUVE EN IMPESANTEURBOULAY JL; MAULARD J.1972; OFF. NATION. ET. RECH. AEROSPAT., NOTES TECH.; FR.; DA. 1972; NO 197; PP. 1-56; ABS. ANGL.; BIBL. 2 P. 1/2Serial Issue

STAND UND GEGENWAERTIGE ENTWICKLUNG DER STEUERUNG FUER RAUMFAHRZEUGE = SITUATION ACTUELLE ET DEVELOPPEMENT DE LA COMMANDE DES ENGINS SPATIAUXLANDWEHR VON PRAGENAU G.1973; OSTERR. INGR-Z.; OSTERR.; DA. 1973; VOL. 16; NO 2; PP. 56-64; BIBL. 16 REF.Serial Issue

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

METHODE DE MINIMISATION DES ERREURS D'UN SYSTEME DE COMMANDE INERTIELDZHAGAROV GA.1972; IZVEST. VYSSH. UCHEBN. ZAVED., PRIBOROSTR.; S.S.S.R.; DA. 1972; VOL. 15; NO 9; PP. 83-88; BIBL. 2 REF.Serial Issue

ALGORITHME POUR LA DETERMINATION DE LA POSITION D'UN OBJET MOBILEFILARETOVA SA.1973; IZVEST. VYSSH. UCHEBN. ZAVED., PRIBOROSTR.; S.S.S.R.; DA. 1973; VOL. 16; NO 1; PP. 68-71; BIBL. 3 REF.Serial Issue

UTILISATION D'UN FILTRE MATHEMATIQUE POUR LA CONSTRUCTION D'UN SYSTEME INERTIEL SANS PLATE-FORME POUR LA STABILISATION D'UN SPATIONEFSIDOROV IM; GONCHAROVA LE; KOZLOVSKAYA AA et al.1972; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1972; VOL. 10; NO 6; PP. 841-849; BIBL. 4 REF.Serial Issue

A QUASI-INERTIAL ATTITUDE MODE FOR ORBITING SPACECRAFT = UN MODE D'ATTITUDE QUASI INERTIEL POUR VEHICULE SPATIAL SUR ORBITEELROD BD.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 889-895; BIBL. 6 REF.Serial Issue

INERTIAL NAVIGATION COMPONENTS AND SYSTEMS. 15TH. MEETING OF THE GUIDANCE AND CONTROL PANEL OF A.G.A.R.D. PAPERS. FLORENCE, 2-5 OCTOBER 19721973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 116; PP. (413 P.); BIBL. DISSEM.Conference Paper

AEROSPACE SYSTEMS TECHNOLOGY1973; IN: PROC. 6TH HAWAII INT. CONF. SYST. SCI.; HONOLULU; 1973; S.L.; WESTERN PERIODICALS; DA. 1973; VOL. 1; PP. 452-473; BIBL. DISSEM.Conference Paper

DER DEUTSCHE AERONOMIESATELLIT AEROS = LE SATELLITE ALLEMAND D'AERONOMIE AEROSPICKER U; BACHOR E; SOPPA P et al.1973; RAUMFAHRTFORSCHUNG; DTSCH.; DA. 1973; VOL. 17; NO 2; PP. 49-85; ABS. ANGLSerial Issue

DIGITAL AUTOPILOT FOR THE SKYLAB ORBITAL ASSEMBLYTURNBULL JF.1972; NAVIGATION; U.S.A.; DA. 1972; VOL. 19; NO 3; PP. 281-289Serial Issue

MINIMAX FAILURE DETECTION AND IDENTIFICATION IN REDUNDANT GYRO AND ACCELEROMETER SYSTEMS = DETECTION DE DEFAILLANCE ET IDENTIFICATION MINIMALE DANS DES SYSTEMES REDONDANTS DE GYROS ET D'ACCELEROMETRESPOTTER JE; DECKERT JC.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 4; PP. 236-243; BIBL. 11 REF.Serial Issue

ESTIMATING TRAJECTORY CORRECTION REQUIREMENTS FOR MULTIPLE OUTER PLANET MISSIONSFRIEDMAN LD; HAMILTON TW; STANTON RH et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 909-914; BIBL. 10 REF.Serial Issue

INTEGRATED NAVIGATION SYSTEMS AND KALMAN FILTERING: A PERSPECTIVE = LES SYSTEMES DE NAVIGATION INTEGRES ET LE FILTRAGE DE KALMAN: UNE PERSPECTIVEBROWN RG.1972; NAVIGATION; U.S.A.; DA. 1972; VOL. 19; NO 4; PP. 355-362; BIBL. 6 REF.Serial Issue

THE CONJUGATE GRADIENT METHOD AND ITS APPLICATIONS TO AEROSPACE VEHICLE GUIDANCE AND CONTROL. I. BASIC RESULTS IN THE CONJUGATE GRADIENT METHOD = LA METHODE DU GRADIENT CONJUGUE ET SON APPLICATION AU GUIDAGE ET A LA COMMANDE DE VEHICULES AEROSPATIAUX. I. RESULTATS FONDAMENTAUX DANS LA METHODE DU GRADIENT CONJUGUELEONDES CT; WU CA.1972; ASTRONAUT. ACTA; G.B.; DA. 1972; VOL. 17; NO 6; PP. 871-880; ABS. FR. ALLEM.; BIBL. 15 REF.Serial Issue

RENDEZVOUS PROBLEM = PROBLEMES DE RENDEZ-VOUSHOUBOLT JC.1966; IN: SPACE MATH. PROC. SUMMER SEMIN. ITHACA, N.Y., 1963; PROVIDENCE, R.I.; AM. MATH. SOC.; DA. 1966; PP. 276-301Conference Proceedings