SINGLE-CHANNEL WHITE-NOISE ESTIMATORS FOR DECONVOLUTION.MENDEL JM; KORMYLO J.1978; GEOPHYSICS; U.S.A.; DA. 1978; VOL. 43; NO 1; PP. 102-124; BIBL. 40 REF.Article

MANOEUVRE HANDLING IN A MULTIRADAR, A.T.C. SYSTEMTHOMAS HW.1979; PROC. INSTIT. ELECTR. ENGRS; GBR; DA. 1979; VOL. 126; NO 6; PP. 469-475; BIBL. 3 REF.Article

PRESUPPOSITION IN BINARY AND FUZZY LOGICSYAGER RR.1983; KYBERNETES; ISSN 0368-492X; GBR; DA. 1983; VOL. 12; NO 2; PP. 135-139; BIBL. 3 REF.Article

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

PERFORMANCE SENSITIVITY OF THE KALMAN FILTER TO CHOICE OF STATE AND OBSERVATION VECTORSCOOKE CC.1981; MATH. COMPUT. SIMUL.; ISSN 0378-4754; NLD; DA. 1981; VOL. 23; NO 2; PP. 199-205; BIBL. 8 REF.Article

DATA COMPRESSION IN KALMAN FILTERINGBAR ITZHACK IY.1979; ISRAEL ANNULATION CONFERENCE ON AVIATION AND ASTRONAUTICS. 21/1979-02-28/TEL-AVIV, HAIFA; ISR; HAIFA: AYALON OFFSET; DA. 1979; PP. 104-110; BIBL. 15 REF.Conference Paper

PARAMETER ESTIMATION VIA THE KALMAN FILTER.AIDALA VJ.1977; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1977; VOL. 22; NO 3; PP. 471-472; BIBL. 4 REF.Article

STEADY STATE RESULTS FOR THE X, Y, Z KALMAN TRACKING FILTER.RAMACHANDRA KV; SRINIVASAN VS.1977; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1977; VOL. 13; NO 4; PP. 419-423; BIBL. 2 REF.Article

FILTRATION MULTI-CANAL ET TRIDIMENSIONNELLE KALMAN DU SIGNAL SISMIQUEWOJCIK P.1977; NAFTA; POLSKA; DA. 1977; VOL. 33; NO 6; PP. 194-197; ABS. RUSSE ANGL.; BIBL. 11 REF.Article

VOYAGER ORBIT DETERMINATION AT JUPITER = DETERMINATION DE L'ORBITE DE "VOYAGER" PRES DE JUPITERCAMPBELL JK; SYNNOTT SP; BIERMAN GJ et al.1983; IEEE TRANSACTIONS ON AUTOMATIC CONTROL; ISSN 0018-9286; USA; DA. 1983; VOL. 28; NO 3; PP. 256-268; BIBL. 15 REF.Article

TWO-DIMENSIONAL KALMAN FILTERINGWOODS JW.1981; TOPICS APPL. PHYS.; DEU; DA. 1981; VOL. 42; PP. 155-205; BIBL. 26 REF.Article

DETECTION OF ABRUPT CHANGE AND TREND IN THE TIME SERIES = DETECTION D'UN CHANGEMENT ABRUPT ET D'UNE TENDANCE DANS LES SERIES TEMPORELLESISHII N; IWATA A; SUZUMURA N et al.1980; INTERNATION. J. SYST. SCI.; GBR; DA. 1980; VOL. 11; NO 5; PP. 557-566; BIBL. 4 REF.Article

GENERALISED DECISION FEEDBACK EQUALISATION OF DIGITAL COMMUNICATION CHANNELSDALLE MESE E; GIULI D.1979; IEE J. ELECTRON. CIRCUITS SYST.; GBR; DA. 1979; VOL. 3; NO 4; PP. 145-152; ABS. ITA; BIBL. 46 REF.Article

ALGORITHME D'ADAPTATION D'UN FILTRE DE KALMANKOVAL'CHUK IA; GORBUNOV AP.1979; IZVEST. VYSSH. UCHEBN. ZAVED., RADIOELEKTRON.; UKR; DA. 1979; VOL. 22; NO 8; PP. 23-28; BIBL. 7 REF.Article

ADAPTIVE IMAGE FILTERINGCHEN CH.1979; PATTERN RECOGNITION AND IMAGE PROCESSING. INSTITUTE OF ELECTRICAL AND ELECTRONICS ENGINEERS COMPUTER SOCIETY. CONFERENCE ON PATTERN RECOGNITION AND IMAGE PROCESSING/1979/CHICAGO IL; USA; NEW YORK: IEEE; DA. 1979; PP. 32-37; BIBL. 12 REF.Conference Paper

FILTERING AND ERROR ANALYSIS VIA THE UDU COVARIANCE FACTORIZATIONTHORNTON CL; BIERMAN GJ.1978; I.E.E.E. TRANS. AUTOMAT. CONTROL; USA; DA. 1978; VOL. 23; NO 5; PP. 901-907; BIBL. 15 REF.Article

A NEW CONSERVATION LAW FOR LINEAR FILTERING PROCESSESCASTI J.1978; J. OPTIMIZ. THEORY APPL.; USA; DA. 1978; VOL. 25; NO 4; PP. 591-595; BIBL. 4 REF.Article

ON THE STATE AND PARAMETER ESTIMATION FOR MANEUVERING REENTRY VEHICLES.CHAW BING CHANG; WHITHING RH; ATHANS M et al.1977; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1977; VOL. 22; NO 1; PP. 99-105; BIBL. 21 REF.Article

GRAM-SCHMIDT ALGORITHMS FOR COVARIANCE PROPAGATION.THORNTON CL; BIERMAN GJ.1975; IN: CONF. DECIS. CONTROL. SYMP. ADAPT. PROCESSES. 14. PROC.; HOUSTON, TEX.; 1975; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1975; PP. 489-498; BIBL. 10 REF.Conference Paper

THE EXTENDED. KALMAN FILTER AS A PULMONARY BLOOD FLOW ESTIMATOR = LE FILTRE DE KALMAN ETENDU COMME UN ESTIMATEUR DU DEBIT SANGUIN PULMONAIREBROVKO O; WIBERG DM; ARENA L et al.1981; AUTOMATICA (OXF.); ISSN 0005-1098; GBR; DA. 1981; VOL. 17; NO 1; PP. 213-220; BIBL. 17 REF.Article

EXPERIENCES IN THE DEVELOPMENT OF AIDED INS DOR AIRCRAFT.SCHMIDT SF.1976; AGARD-LS-82; FR.; DA. 1976; PP. I.1-I.21; BIBL. 10 REF.; (PRACT. ASPECTS KALMAN FILTERING IMPLEMENTATION)Report

FILTER STABILITY FOR STOCHASTIC EVOLUTION EQUATIONS.VINTER RB.1976; IN: CONF. DECIS. CONTROL. SYMP. ADAPT. PROCESSES. 15. PROC.; CLEARWATER, FLA.; 1976; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1976; PP. 1126-1128; BIBL. 7 REF.Conference Paper

PRATICAL ASPECTS OF KALMAN FILTERING IMPLEMENTATION.1976; AGARD-LS-82; FR.; DA. 1976; PP. (179P.); BIBL. DISSEM.; ISBN 9283501608Report

MULTICONFIGURATION KALMAN FILTER DESIGN FOR HIGH-PERFORMANCE GPS NAVIGATION = SYNTHESE DU FILTRE DE KALMAN A CONFIGURATIONS MULTIPLES POUR LA NAVIGATION AVEC UN SYSTEME DE REPERAGE GLOBAL A HAUTE PERFORMANCEKAO MH; ELLER DH.1983; IEEE TRANSACTIONS ON AUTOMATIC CONTROL; ISSN 0018-9286; USA; DA. 1983; VOL. 28; NO 3; PP. 304-314; BIBL. 25 REF.Article

ADVANCES IN THE TECHNIQUES AND TECHNOLOGY OF THE APPLICATION OF NONLINEAR FILTERS AND KALMAN FILTERSLEONDES CT ED.1982; ; FRA; NEUILLY-SUR-SEINE: AGARD; DA. 1982; AGARD/AG-256; 538 P.; 30 CM; ISBN 92-835-1418-1; AGARDOGRAPH; 256Report