A NOTE ON KALMAN-BUCY FILTERS WITH ZERO MEASUREMENT NOISE. = NOTE SUR LES FILTRES DE KALMAN-BUCY AVEC BRUIT DE MESURE NULMOYLAN PJ.1974; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1974; VOL. 19; NO 3; PP. 263-264; BIBL. 3 REF.Article

A NEW SEQUENTIAL ESTIMATOR FOR NON-LINEAR MODELSLEUNG VP; PADMANABHAN L.1972; INTERNATION. J. SYST. SCI.; G.B.; DA. 1972; VOL. 3; NO 4; PP. 395-406; BIBL. 7 REF.Serial Issue

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

FILTRAGE ET LISSAGE STATISTIQUES OPTIMAUXRADIX JC.1982; MESURES ET CONTROLE; FRA; PARIS: TECHNIQUES DE L'INGENIEUR; DA. 1982; NO 79; R7425; PP. 1-17; BIBL. 15 REF.Book Chapter

ESTIMATION I1972; IN: PROC. I.E.E.E. CONF. DECIS. CONTROL 11TH SYMP. ADAPT. PROCESSES; NEW ORLEANS, LA; 1972; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1972; PP. 201-223; BIBL. DISSEM.Conference Paper

ESTIMATION II1972; IN: PROC. I.E.E.E. CONF. DECIS. CONTROL 11TH SYMP. ADAPT. PROCESSES; NEW ORLEANS, LA; 1972; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1972; PP. 647-671; BIBL. DISSEM.Conference Paper

ADAPTIVE PARAMETER IDENTIFICATION = IDENTIFICATION ADAPTATIVE DE PARAMETREKAUFMAN H; BEAULIER D.1972; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1972; VOL. 17; NO 5; PP. 729-731; BIBL. 2 REF.Serial Issue

APPLICATIONS OF NONLINEAR FILTERING TECHNIQUES TO AEROSPACE VEHICLE TRACKING AND PARAMETER IDENTIFICATIONLARSON RE.sdIN: THEOR. PRAT. IDENTIFICATION MODELISATION SYST. EC. ETE AUTOM. TOULOUSE, 1972; S.L.; DA. S.D.; PP. (91 P.); BIBL. 14 REF.Conference Paper

ON EXTENDED KALMAN FILTER AS A PARAMETER ESTIMATOR FOR LINEAR SYSTEMS WITH CORRELATED NOISEELKOBROSY GA.1982; CONTROL COMPUT.; ISSN 0730-9538; USA; DA. 1982; VOL. 10; NO 3; PP. 76-80; BIBL. 15 REF.Article

A SHIP TRACKING SYSTEM USING A KALMAN-SCHMIDT FILTER.DARMON CA.1976; AGARD-LS-82; FR.; DA. 1976; PP. 6.1-6.24; BIBL. 6 REF.; (PRACT. ASPECTS KALMAN FILTERING IMPLEMENTATION)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

DIGITAL ADAPTIVE MODEL FOLLOWING FLIGHT CONTROL.ALAG GS; KAUFMAN H.1974; IN: AIAA MECH. CONTROL FLIGHT CONF.; ANAHEIM, CALIF.; 1974; NEW YORK; AIAA; DA. 1974; VOL. 886; PP. 1-7; BIBL. 11 REF.Conference Paper

MANAGEMENT OF ANALYTICAL REDUNDANCY IN DIGITAL FLIGHT CONTROL SYSTEMS FOR AIRCRAFT.MONTGOMERY RC; PRICE DB.1974; IN: AIAA MECH. CONTROL FLIGHT CONF.; ANAHEIM, CALIF.; 1974; NEW YORK; AIAA; DA. 1974; VOL. 887; PP. 1-10; BIBL. 4 REF.Conference Paper

ZUR ANWENDUNG DES KALMAN-FILTERS. = SUR L'UTILISATION DU FILTRE DE KALMANKROGMANN U.1974; INTERNATION. ELEKTRON. RDSCH.; DTSCH.; DA. 1974; VOL. 28; NO 8; PP. 167-171; ABS. ANGL. FRArticle

A VARIABLE STEP ALGORITHM TO AID CONVERGENCE OF THE ITERATED EXTENDED KALMAN FILTER FOR USE IN A NAVIGATION SATELLITE PROBLEM.JANOSKO RE.1974; IN: AIAA MECH. CONTROL FLIGHT CONF.; ANAHEIM, CALIF.; 1974; NEW YORK; AIAA; DA. 1974; VOL. 807; PP. 1-8; BIBL. 8 REF.Conference Paper

INFLUENCE DE LA REGULARISATION SUR LA PRECISION DE L'ESTIMATION DANS LES FILTRES RECURRENTSRYABOVA ORESHKOVA AP.1972; IZVEST. AKAD. NAUK S.S.S.R., TEKH. KIBERN.; S.S.S.R.; DA. 1972; NO 5; PP. 202-206; BIBL. 4 REF.Serial Issue

MINIMIERUNG EINER FEHLERQUADRATSUMME IN EINZELSCHRITTEN. = MINIMISATION D'UNE SOMME DE CARRES D'ERREURS PAR ETAPES INDIVIDUELLESBOSSE G.1975; FREQUENZ; DTSCH.; DA. 1975; VOL. 29; NO 6; PP. 178-181; ABS. ANGL.; BIBL. 3 REF.Article

ADAPTIVE ESTIMATION VIA SEQUENTIAL PROCESSING.HAWKES RM; MOORE JB.1975; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1975; VOL. 20; NO 1; PP. 137-138; BIBL. 7 REF.Article

CHANNEL EQUALIZATION USING A KALMAN FILTER FOR PAST DATA TRANSMISSION.GODARD D.1974; I.B.M. J. RES. DEVELOP.; U.S.A.; DA. 1974; VOL. 18; NO 3; PP. 267-273; BIBL. 15 REF.Article

RECURSIVE FADING MEMORY SMOOTHINGSACKS JE; SORENSON HW.1973; INFORM. SCI.; U.S.A.; DA. 1973; VOL. 5; PP. 45-61; BIBL. 18 REF.Serial Issue

SPEECH DATE RATE REDUCTION. II. SENSITIVITY AND ERRORGUNN JE; SAGE AP.1973; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1973; VOL. 9; NO 2; PP. 139-150; BIBL. 13 REF.Serial Issue

ON THE COMPUTATION OF KALMAN GAIUS.TAYLOR FJ.1975; COMPUTERS ELECTR. ENGNG; G.B.; DA. 1975; VOL. 2; NO 1; PP. 105-115; BIBL. 6 REF.Article

A COMPARISON OF COMPLEMENTARY AND KALMAN FILTERING.HAGGINS WT JR.1975; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1975; VOL. 11; NO 3; PP. 321-325; BIBL. 7 REF.Article

A DIGITAL KALMAN FILTER FOR RADAR TRACKING WITH FILTER GAINS INDEPENDENT OF SAMPLING INTERVAL.CHIDAMBARA MR; SHIVAPRASAD AP.1974; J. INDIAN INST. SCI.; INDIA; DA. 1974; VOL. 56; NO 8-10; PP. 409-421; BIBL. 5 REF.Article

ENLARGING THE REGION OF CONVERGENCE OF KALMAN FILTERS EMPLOYING RANGE MEASUREMENTSWIDNALL WS.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 283-287; BIBL. 4 REF.Serial Issue