kw.\*:("AUTOMATIC STEERER")
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PRELIMINARY CONTROL SYSTEM USING PREFERRED FEEDBACK STATES.CHERONIS CG.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 7; PP. 609-610Article
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
VERIFICATION OF DIGITAL AUTOPILOT SOFTWARE PERFORMANCEGILBERT RW.1982; INSTITUTE OF ELECTRICAL AND ELECTRONIC ENGINEERS. SOUTHEASTCON '82 CONFERENCE/1982-04-04/DESTIN FL; USA; NEW YORK: IEEE; DA. 1982; PP. 384-385; BIBL. 2 REF.Conference Paper
EVOLUTION OF TITAN FAMILY GUIDANCE AND CONTROL SYSTEMSTURCO JA.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 161-162Conference Paper
SHUTTLE AUTOMATIC LANDING SYSTEMTSIKALAS G; DYER D.1982; ADV. ASTRONAUT. SCI.; ISSN 0065-3438; USA; DA. 1982; VOL. 48; PP. 121-140Conference Paper
MINI-RPV LATERAL AUTOPILOT DESIGN.BAR ITZHACK IY; FERDMAN E.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 9; PP. 1189-1195; BIBL. 11 REF.Article
CORRECTIONS D'ORBITES D'UN SATELLITE GEOSYNCHRONE: ETUDE DES EFFETS INDUITS DANS LE PLAN DE L'ORBITE PAR DES CORRECTIONS NORD-SUD.ESTERLE A.1976; CENTRE NATION. ET. SPATIALES, NOTE TECH.; FR.; DA. 1976; NO 41; PP. 1-34; ABS. ANGL.; BIBL. 2 REF.Serial Issue
DESIGN OF SHIP STEERING AUTOPILOTS BY QUADRATIC SYNTHESISTRANKLE TL.1980; ASILOMAR CONFERENCE ON CIRCUITS, SYSTEMS & COMPUTERS. 13/1979/PACIFIC GROVE CA; USA; NEW YORK: IEEE; DA. 1980; PP. 69-72; BIBL. 7 REF.Conference Paper
PROGRESS IN THE USE OF AUTOMATIC FLIGHT CONTROLS IN SAFETY CRITICAL APPLICATIONSHOWARD RW.1980; AERONAUT. J.; ISSN 0001-9240; GBR; DA. 1980; VOL. 84; NO 837; PP. 316-326Article
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
Adaptive steering of ships. A model reference approachVAN AMERONGEN, J.Automatica (Oxford). 1984, Vol 20, Num 1, pp 3-14, issn 0005-1098Article
AUTOPILOT DESIGN VIA IMPROVED DISCRETE MODAL CONTROLSTALLARD DV.1981; GUIDANCE AND CONTROL CONFERENCE/1981/ALBUQUERQUE NM; USA; NEW-YORK: AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS; DA. 1981; PP. 162-172; BIBL. 43 REF.Conference Paper
CONTROL DESIGN FOR REDUCTION OF AERODYNAMIC TAIL FORCES USING QUADRATIC SYNTHESISHOLLEY WE; WEI SY.1980; ASILOMAR CONFERENCE ON CIRCUITS, SYSTEMS & COMPUTERS. 13/1979/PACIFIC GROVE CA; USA; NEW YORK: IEEE; DA. 1980; PP. 73-77; BIBL. 11 REF.Conference Paper
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
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
IMPLEMENTATION OF AN ADAPTIVE AUTOPILOT SCHEME FOR THE F-8 AIRCRAFT USING THE ADAPTIVE-PREDICTIVE CONTROL SYSTEMMARTIN SANCHEZ JM.1980; ASILOMAR CONFERENCE ON CIRCUITS, SYSTEMS & COMPUTERS. 13/1979/PACIFIC GROVE CA; USA; NEW YORK: IEEE; DA. 1980; PP. 606-610; BIBL. 8 REF.Conference Paper
ZUR OPTIMALEN ANWENDUNG DES KURSREGLERS (SELBSTEUERS) = UTILISATION OPTIMALE DU PILOTE AUTOMATIQUEEBERT EP; BISKOP H; BERKING B et al.1979; SCHIFF U. HAFEN; DEU; DA. 1979; VOL. 31; NO 8; PP. 705-708; BIBL. 8 REF.Article
SERVOMECANISMES D'AVIONS SUPERSONIQUES.MARIN B.1977; AUTOMAT. INFORMAT. INDUSTR.; FR.; DA. 1977; NO 58; PP. 33-40; BIBL. 8 REF.Article
SUR LES CRITERES D'INSTABILITE DU GOUVERNAIL D'AUTOPILOTE, ANALYSE DE LA REPONSE EN FREQUENCE ET CONSIDERATION DE BASEHASEGAWA K; ISHIYAMA T; UMEDA H et al.1980; J. SOC. NAV. ARCHIT. JPN.; ISSN 0514-8499; JPN; DA. 1980-12; VOL. 148; PP. 92-100; ABS. ENG; BIBL. 11 REF.Article
CZLOWIEK I AUTOMATYZACJA = L'HOMME ET L'AUTOMATISATIONSMOLICZ T.1979; POST. ASTRONAUT., BIUL. NAUK; POL; DA. 1979; VOL. 12; NO 2; PP. 53-63; ABS. RUS/ENG; BIBL. 6 REF.Article
LES EQUIPEMENTS ELECTRONIQUES WESMAR A USAGE MARITIME ET FLUVIAL1978; NAV. PORTS CHANTIERS; FRA; DA. 1978; NO 341; PP. 657-662Article
ROBUSTNESS IN LINEAR QUADRATIC FEEDBACK DESIGN WITH APPLICATION TO AN AIRCRAFT CONTROL PROBLEM.PATEL RV; SRIDHAR B; TODA M et al.1977; IN: ANNU. ASILOMAR CONF. CIRCUITS, SYST., COMPUT. 10; PACIFIC GROVE, CALIF.; 1976; NORTH HOLLYWOOD, CALIF.; WESTERN PERIODICALS; DA. 1977; PP. 293-300; BIBL. 9 REF.Conference Paper