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ALOGORITHMS FOR THE WEIGHTING MATRICES IN SAMPLED-DATA LINEAR TIME-INVARIANT OPTIMAL REGULATOR PROBLEMSLEONDES CT; SALAMI MA.1980; COMPUTERS ELECTR. ENGNG; GBR; DA. 1980; VOL. 7; NO 1; PP. 11-23; BIBL. 14 REF.Article

LOWER BOUNDS FOR A QUADRATIC COST FUNCTIONAL.ARONOFF E; LEONDES CT.1976; INTERNATION: J. SYST. SCI.; G.B.; DA. 1976; VOL. 7; NO 1; PP. 17-25; BIBL. 5 REF.Article

OPTIMAL ADAPTIVE CONTROL OF AN ARRAY OF PASSIVE SENSORS.LAU CK; LEONDES CT.1975; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1975; VOL. 11; NO 4; PP. 608-612; BIBL. 7 REF.Article

AN ALGORITHM FOR THE SOLUTION OF DIFFERENTIAL GAMES WITH BOUNDS ON THE STATE AND CONTROL VARIABLES. II. THE APPLICATION OF THE ALGORITHM.LEFFLER N; LEONDES CT.1975; COMPUTERS ELECTR. ENGNG; G.B.; DA. 1975; VOL. 2; NO 1; PP. 83-94Article

ON THE COMPUTATIONAL ADVANTAGES OF STAGEWISE-OPTIMAL OBSERVERS.IGLEHART SC; LEONDES CT.1974; I.E.E.E. TRANS-AUTOMAT. CONTROL; U.S.A.; DA. 1974; VOL. 19; NO 2; PP. 147-149; BIBL. 7 REF.Article

THE CONJUGATE GRADIENT METHOD AND ITS APPLICATION TO AEROSPACE VEHICLE GUIDANCE AND CONTROL. II. MARS ENTRY GUIDANCE AND CONTROL = LA METHODE DU GRADIENT CONJUGUE ET SON APPLICATION AU GUIDAGE ET A LA COMMANDE DE VEHICULES AEROSPATIAUX. II. GUIDAGE ET COMMANDE D'UNE ENTREE DANS L'ATMOSPHERE DE MARSLEONDES CT; WU CA.1972; ASTRONAUT. ACTA; G.B.; DA. 1972; VOL. 17; NO 6; PP. 881-890; ABS. FR. ALLEM.; BIBL. 17 REF.Serial Issue

ON DISCRET-TIME RICCATI-LIKE MATRIX DIFFERENCE EQUATIONS WITH RANDOM COEFFICIENTSPANOSSIAN H; LEONDES CT.1983; INTERNATIONAL JOURNAL OF SYSTEMS SCIENCE; ISSN 0020-7721; GBR; DA. 1983; VOL. 14; NO 4; PP. 385-407; BIBL. 36 REF.Article

APPLICATION OF SINGULAR PERTURBATIONS TO OPTIMAL CONTROLKRIKORIAN KV; LEONDES CT.1982; CONTROL DYN. SYST.; ISSN 0090-5267; USA; DA. 1982; VOL. 18; PP. 131-160; BIBL. 22 REF.Article

PAYOFF SENSITIVITY OF LINEAR QUADRATIC DIFFERENTIAL GAMES TO PARAMETER CHANGE = SENSIBILITE DE GAIN DES JEUX DIFFERENTIELS LINEAIRES QUADRATIQUES A UNE VARIATION DE PARAMETRESLEONDES CT; SUI TK.1981; J. DYN. SYST., MEAS., CONTROL; ISSN 0022-0434; USA; DA. 1981; VOL. 103; NO 1; PP. 36-38; BIBL. 8 REF.Article

ON-LINE SOLUTION OF A STOCHASTIC PURSUIT EVASION GAMELEONDES CT; MONS B.1979; J. OPTIMIZ. THEORY APPL.; USA; DA. 1979; VOL. 28; NO 3; PP. 411-428; BIBL. 4 REF.Article

POLE ASSIGNMENT BY PICEWISE CONSTANT OUTPUT FEEDBACKCHAMMAS AB; LEONDES CT.1979; INTERNATION. J. CONTROL; GBR; DA. 1979; VOL. 29; NO 1; PP. 31-38; BIBL. 4 REF.Article

ON THE DESIGN OF LINEAR TIME INVARIANT SYSTEMS BY PERIODIC OUTPUT FEEDBACK. I. DISCRETE-TIME POLE ASSIGNMENTCHAMMAS AB; LEONDES CT.1978; INTERNATION. J. CONTROL; GBR; DA. 1978; VOL. 27; NO 6; PP. 885-894; BIBL. 12 REF.Article

VOLTERRA SERIES SYNTHESIS OF NONLINEAR STOCHASTIC TRACKING SYSTEMS.LANDAU M; LEONDES CT.1975; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1975; VOL. 11; NO 2; PP. 245-265; BIBL. 7 REF.Article

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

MULTISTAGE STOCHASTIC LINEAR DIFFERENTIAL GAME WITH DECISION-TIME CONSTRAINTLAU CK; LEONDES CT.1982; INT. J. SYST. SCI.; ISSN 0020-7721; GBR; DA. 1982; VOL. 15; NO 9; PP. 1047-1060; BIBL. 18 REF.Article

IDENTIFICATION BOTH OF THE UNKNOWN PLANT AND NOISE PARAMETERS OF THE KALMAN FILTER = IDENTIFICATION DES PARAMETRES INCONNUS DU SYSTEME ET DU BRUIT DU FILTRE DE KALMANLEONDES CT; SIU TK.1980; INTERNATION. J. SYST. SCI.; GBR; DA. 1980; VOL. 11; NO 6; PP. 711-720; BIBL. 13 REF.Article

ON THE DESIGN OF LINEAR TIME-INVARIANT SYSTEMS BY PERIODIC OUTPUT FEEDBACK. II. OUTPUT FEEDBACK CONTROLLABILITYCHAMMAS AB; LEONDES CT.1978; INTERNATION. J. CONTROL; GBR; DA. 1978; VOL. 27; NO 6; PP. 895-903; BIBL. 5 REF.Article

LEAST SQUARES ESTIMATION OF NONSTATIONARY COVARIANCE PARAMETERS IN LINEAR SYSTEMS.BREWER HW; LEONDES CT.1977; AUTOMATICA; G.B.; DA. 1977; VOL. 13; NO 3; PP. 265-277; BIBL. 13 REF.Article

PARAMETER ESTIMATION OF NONLINEAR TIME-VARIANT SYSTEMS BY THE METHOD OF SENSITIVITY FUNCTIONS.DURANDO AR; LEONDES CT.1976; COMPUTERS ELECTR. ENGNG.; G.B.; DA. 1976; VOL. 3; NO 4; PP. 421-424; BIBL. 4 REF.Article

A TREATMENT OF NONWHITE MEASUREMENT NOISE IN DISCRETE LINEAR SYSTEMS.BREWER HW; LEONDES CT.1976; AUTOMATICA; G.B.; DA. 1976; VOL. 12; NO 4; PP. 371-374; BIBL. 7 REF.Article

AN ALGORITHM FOR THE SOLUTION OF DIFFERENTIAL GAMES WITH BOUNDS ON THE STATE AND CONTROL VARIABLE. I. THE DEVELOPMENT OF ALGORITHM.LEFFLER N; LEONDES CT.1975; COMPUTERS ELECTR. ENGNG; G.B.; DA. 1975; VOL. 2; NO 1; PP. 67-81; BIBL. 5 REF.Article

KALMAN FILTERING OF SYSTEMS WITH PARAMETER UNCERTAINTIES. A SURVEYLEONDES CT; PEARSON JO.1973; INTERNATION. J. CONTROL; G.B.; DA. 1973; VOL. 17; NO 4; PP. 785-801; BIBL. 1 P.Serial Issue

DECENTRALIZED CONTROL OF DISCRETE TIME LINEAR SYSTEM WITH INCOMPLETE INFORMATIONCHAMMAS AB; LEONDES CT.1982; INTERNATIONAL JOURNAL OF CONTROL; ISSN 0020-7179; GBR; DA. 1982; VOL. 36; NO 4; PP. 575-595; BIBL. 14 REF.Article

DYNAMIC PROGRAMMING USING SINGULAR PERTURBATIONS = PROGRAMMATION DYNAMIQUE UTILISANT LES PERTURBATIONS SINGULIERESKRIKORIA KV; LEONDES CT.1982; J. OPTIM. THEORY APPL.; ISSN 0022-3239; USA; DA. 1982; VOL. 38; NO 2; PP. 221-230; BIBL. 12 REF.Article

SYNTHESIS OF A HIGH-SPEED TRACKED VEHICLE SUSPENSION SYSTEM. I. PROBLEM STATEMENT, SUSPENSION STRUCTURE, AND DECOMPOSITION.GUENTHER CR; LEONDES CT.1977; I.E.E.E. TRANS. AUTOMAT. CONTROL; U.S.A.; DA. 1977; VOL. 22; NO 2; PP. 158-165Article

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