Les nouveaux radar et gyropilote Sperry = The new radar and Sperry gyropilotNavires, Ports et Chantiers. 1985, Vol 36, Num 419, pp 189-192, issn 0028-159XArticle

An optimal controller arising from minimization of a quadratic performance criterion of indefinite formREID, R. E; TUGCU, A. K; MEARS, B. C et al.IEEE transactions on automatic control. 1983, Vol 28, Num 10, pp 985-987, issn 0018-9286Article

Adaptive steering of ships. A model reference approachVAN AMERONGEN, J.Automatica (Oxford). 1984, Vol 20, Num 1, pp 3-14, issn 0005-1098Article

Pilote automatique: une technologie à des fins militaires et civiles = Automatic steerer: one technology for military or civil applicationsNavires, Ports et Chantiers. 1985, Vol 36, Num 425, pp 560-561, issn 0028-159XArticle

Automatic pilotage of large ships in confined waters: a multivariable approachBURNS, R. S; DOVE, M. J; BOUNCER, T. H et al.Application of multivariable systems theory. Symposium. 1982, pp 71-80Conference Paper

Neural network prediction of the wave influence on the yaw motion of a shipNICOLAU, Viorel; AIORDACHIOAIE, Dorel; POPA, Rustem et al.International Joint Conference on Neural Networks. 2004, isbn 0-7803-8359-1, 4Vol, Vol4, 2801-2806Conference Paper

Signalisation du métro de Caracas: particularités fonctionnelles et de réalisation = Signalling system for Caracas metro: functional and realisation particularitiesSCHNEIDER, J.-P; COLLARD, J.-L; DUTERTRE, J.-L et al.Revue générale des chemins de fer (1924). 1985, Vol 104, pp 103-112, issn 0035-3183Article

Approche générique H-infini/nu pour la synthèse et l'analyse d'un pilote automatique de missile soumis à une aéroélasticité importante = H-infinity/nu generic approach for the synthesis and analysis of a missile autopilot subject to a strong aeroelasticityFriang, Jean-Patrick; Duc, G.1996, 193 p.Thesis

Optimal dual-rate digital redesign with application to missile controlRABBATH, C. A; LECHEVIN, N; HORI, N et al.Journal of guidance, control, and dynamics. 2004, Vol 27, Num 6, pp 1083-1087, issn 0731-5090, 5 p.Article

Robust autopilot design for ship steering in wavesZHANG, R; SUN, Z; XU, H et al.International shipbuilding progress. 1997, Vol 44, Num 437, pp 59-75, issn 0020-868XArticle

Un essai multiaxial automatique pour la caractérisation des bétonsCLEMENT, J.-L; RAMTANI, S.Les Cahiers de rhéologie (Paris). 1991, Vol 9, Num 2, pp 61-70, issn 1149-0039Article

A stochastic rudder control law for ship path-following autopilotsRIOS-NETO, A; DA CRUZ, J. J.Automatica (Oxford). 1985, Vol 21, Num 4, pp 371-384, issn 0005-1098Article

La simulation dans les transportsBUQUET, A; PERRIN, J.-P.T.E.C. (Paris). 1984, Num 64, pp 25-30, issn 0397-6513Article

A COMPARISON OF THREE COMPUTERIZED DESIGN ALGORITHMS FOR CONTROL SYSTEMS.CASE TW; MITCHELL JR; MCDANIEL WL JR et al.1976; IN: ANNU. SOUTHEAST. SYMP. SYST. THEORY. 8. PROC.; KNOXVILLE, TENN.; 1976; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1976; PP. 259-263; BIBL. 5 REF.Conference Paper

A HISTORICAL REVIEW OF AUTOPILOT DEVELOPMENT, RESEARCH, AND THEORY IN GERMANY.OPPELT W.1976; J. DYNAM. SYST. MEASUR. CONTROL; U.S.A.; DA. 1976; VOL. 98; NO 3; PP. 215-223; BIBL. 1 P. 1/2Article

PRELIMINARY CONTROL SYSTEM USING PREFERRED FEEDBACK STATES.CHERONIS CG.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 609-610Article

NEAR-HOVER CONTROL OF A HELICOPTER WITH A HANGING LOAD.GUPTA NK; BRYSON AE JR.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 3; PP. 217-222; BIBL. 18 REF.Article

DIGITAL AUTOPILOT FOR THE SKYLAB ORBITAL ASSEMBLYTURNBULL JF.sdIN: INST. NAVIG. PROC. NATL SPACE MEET. ORLANDO, FLA, 1972; WASHINGTON, D.C.; INST. NAVIG.; DA. S.D.; PP. 63-71Conference Proceedings

Commande modale d'un avion sans pilote par retour dynamique de sortie = Numerical autopilot design by eigen structure assignmentBsalis, Elias; Bucharles, Alain.1992, 328 p.Thesis

CONTROL LOGIC FOR LANDING-ABORT AUTOPILOT MODEETKIN B; SHANGXIANG ZHU.1982; UTIAS REP.; ISSN 0082-5255; CAN; DA. 1982; NO 258; 82 P.; BIBL. 11 REF.Serial Issue

AUTOPILOT LOGIC AN UNMANNED RESEARCH SUBMERSIBLEFULLER JW; TRANKLE TL.1982; INSTITUTE OF ELECTRICAL AND ELECTRONIC ENGINEERS. SOUTHEASTCON '82 CONFERENCE/1982-04-04/DESTIN FL; USA; NEW YORK: IEEE; DA. 1982; PP. 154-156; BIBL. 5 REF.Conference Paper

CHARACTERISTIC FREQUENCY-GAIN DESIGN STUDY OF AN AUTOMATIC FLIGHT CONTROL SYSTEMKOUVARITAKIS B; MURRAY W; MACFARLANE AGJ et al.1979; INTERNATION. J. CONTROL; GBR; DA. 1979; VOL. 29; NO 2; PP. 325-357; BIBL. 11 REF.Article

LENKMASCHINE ZUR UNTERSUCHUNG DER FAHRDYNAMIK VON KRAFTFAHRZEUGEN. = PILOTE AUTOMATIQUE POUR L'ETUDE DE LA DYNAMIQUE DE MARCHE DES VEHICULES AUTOMOBILESPAULY A.1977; AUTOM.-TECH. 2; DTSCH.; DA. 1977; VOL. 79; NO 7-8; PP. 307-310; ABS. ANGL.; BIBL. 4 REF.Article

AUTOMATIC HOVER CONTROL OF AN UNMANNED TETHERED ROTORPLATFORM.SCHMIDT G; SWIK R.1974; AUTOMATICA; G.B.; DA. 1974; VOL. 10; NO 4; PP. 393-403; H.T. 2; ABS. FR. ALLEM. RUSSE; BIBL. 7 REF.Article

PILOTAGE ET CONCEPTION DES AVIONSWANNER JC.1973; AERONAUT. ET ASTRONAUT.; FR.; DA. 1973; NO 40; PP. 10-18; ABS. ANGL. ALLEM.; BIBL. 4 REF.Serial Issue