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SOFTWARE TECHNIQUES FOR SENSOR REDUNDANCY MANAGEMENT OF FLIGHT CONTROL SYSTEMS.SHAPIRO EY.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 632-638; BIBL. 6 REF.Article

ALGORITHMIC PROGRAM DIAGNOSISSHAPIRO EY.1982; ANNUAL ASSOCIATION FOR COMPUTING MACHINERY SYMPOSIUM ON PRINCIPLES OF PROGRAMMING LANGUAGES. 9/1982-01-25/ALBUQUERQUE NM; USA; NEW YORK: ACM; DA. 1982; PP. 299-308; BIBL. 23 REF.Conference Paper

ON THE DESIGN OF SUBOPTIMAL CONTROLLERS FOR MINIMAL TIME FEEDBACK REGULATORS.SHAPIRO EY.1976; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; U.S.A.; DA. 1976; VOL. 12; NO 4; PP. 434-438; BIBL. 19 REF.Article

DESIGN OF FLIGHT CONTROL SYSTEMS USING OPTIMAL OUTPUT CONSTANT FEEDBACK CONTROLLERSSHAPIRO EY; FREDERICKS DA.1979; ICCS 79. INTERNATIONAL CONFERENCE ON CYBERNETICS AND SOCIETY/1979/DENVER CO; USA; NEW YORK: IEEE; DA. 1979; PP. 274-279; BIBL. 12 REF.Conference Paper

GENERALIZED INVERSE OF A MATRIX: THE MINIMIZATION APPROACH.SHAPIRO EY; DECARLI HE.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 10; PP. 1483-1484; BIBL. 4 REF.Article

APPLICATION OF CONSTRAINED CONSTANT OPTIMAL OUTPUT FEEDBACK TO MODERN FLIGHT CONTROL SYNTHESISSHAPIRO EY; FREDRICKS DA.1981; LECT. NOTES CONTROL INF. SCI.; ISSN 0170-8643; DEU; DA. 1981 PUBL. 1982; VOL. 38; PP. 302-310; BIBL. 12 REF.Conference Paper

APPLICATION OF MAXIMUM LIKELIHOOD ESTIMATION TO THE IDENTIFICATION OF THE STABILITY DERIVATIVES OF A WIDE BODY TRANSPORT AIRCRAFTSOBEL KM; SHAPIRO EY.sdANNUAL ALLERTON CONFERENCE ON COMMUNICATION, CONTROL AND COMPUTING. 19/1981/MONTICELLO IL; USA; DA. S.D.; PP. 339-347; BIBL. 9 REF.Conference Paper

APPLICATION OF OPTIMAL CONSTANT OUTPUT FEEDBACK TO FLIGHT CONTROL SYSTEM DESIGNSHAPIRO EY; FREDRICKS DA.sdANNUAL ALLERTON CONFERENCE ON COMMUNICATION, CONTROL, AND COMPUTING. 17/1979/MONTICELLO IL; USA; URBANA-CHAMPAIGN: UNIVERSITY OF ILLINOIS; DA. S.D.; PP. 735-743; BIBL. 12 REF.Conference Paper

ON OUTPUT FEEDBACK DECOUPLING = SUR LE DECOUPLAGE A RETROACTION DE SORTIEKIM HY; SHAPIRO EY.1981; IEEE TRANS. AUTOMAT. CONTROL.; ISSN 0018-9286; USA; DA. 1981; VOL. 26; NO 3; PP. 782-784; BIBL. 7 REF.Article

ON THE GENERATION OF OPTIMAL CONSTANT OUTPUT FEEDBACK GAINS FOR UNSTABLE LINEAR TIME-INVARIANT SYSTEMSSHAPIRO EY; FREDERICKS DA.1979; CONFERENCE ON INFORMATION SCIENCES AND SYSTEMS/1979-03-28/BALTIMORE MD; USA; BALTIMORE: THE JOHNS HOPKINS UNIVERSITY; DA. 1979; PP. 103-108; BIBL. 11 REF.Conference Paper

AN ALGORITHM FOR THE GENERATION OF OPTIMAL CONSTANT OUTPUT FEEDBACK GAINS FOR LINEAR TIME INVARIANT SYSTEMSSHAPIRO EY; FREDRICKS DA.1978; CONFERENCE ON INFORMATION SCIENCES AND SYSTEMS. 12/1978-03-29/BALTIMORE; USA; BALTIMORE: JOHNS HOPKINS UNIVERSITY; DA. 1978; PP. 467-472; BIBL. 14 REF.Conference Paper

ON THE DECOUPLING OF LINEAR SYSTEMS INTO SINGLE INPUT-MULTIPLE OUTPUT SUBSYSTEMSKIM HY; SHAPIRO EY.sdANNUAL ALLERTON CONFERENCE ON COMMUNICATION, CONTROL AND COMPUTING. 19/1981/MONTICELLO IL; USA; DA. S.D.; PP. 144-152; BIBL. 5 REF.Conference Paper

A PRACTICAL ASPECT OF BASS' ALGORITHM FOR STABILIZING LINEAR-TIME-INVARIANT SYSTEMS.SHAPIRO EY; DECARLI HE.1976; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 11; PP. 1630-1631; BIBL. 3 REF.Article

CONSTRAINED EIGENVALUE (EIGENVECTOR) ASSIGNMENT APPLICATION TO FLIGHT CONTROL SYSTEMSSHAPIRO EY; CHUNG JC.sdANNUAL ALLERTON CONFERENCE ON COMMUNICATION, CONTROL AND COMPUTING. 19/1981/MONTICELLO IL; USA; DA. S.D.; PP. 320-328; BIBL. 7 REF.Conference Paper

SUBOPTIMAL CONSTANT OUPTUT FEEDBACK AND ITS APPLICATION TO MODERN FLIGHT CONTROL SYSTEM DESIGN = RETROACTION SOUS OPTIMALE DE SORTIE CONSTANTE ET SON APPLICATION A LA SYNTHESE DES SYSTEMES MODERNES DE COMMANDE DE VOLSHAPIRO EY; FREDRICKS DA; ROONEY RH et al.1981; INT. J. CONTROL; ISSN 0020-7179; GBR; DA. 1981; VOL. 33; NO 3; PP. 505-517; BIBL. 12 REF.Article

RECONSTRUCTED FLIGHT CONTROL SENSOR SIGNALS VIA LUENBERGER OBSERVERSSHAPIRO EY; SCHENK FL; DECARLI HE et al.1979; I.E.E.E. TRANS. AEROSPACE ELECTRON. SYST.; USA; DA. 1979; VOL. 15; NO 2; PP. 245-252; BIBL. 8 REF.Article

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