APPLICATION OF GEOMETRIC DECOUPLING THEORY TO SYNTHESIS OF AIRCRAFT LATERAL CONTROL SYSTEMS = APPLICATION DE LA THEORIE DU DECOUPLAGE GEOMETRIQUE A LA SYNTHESE DE SYSTEMES DE CONTROLE LATERAL D'AVIONSCLIFF EM; LUTZE FH.1972; J. AIRCR.; U.S.A.; DA. 1972; VOL. 9; NO 11; PP. 770-776; BIBL. 15 REF.Serial Issue

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

SAMPLE RATE SELECTION FOR AIRCRAFT DIGITAL CONTROL.POWELL JD; KATZ P.1974; IN: AIAA MECH. CONTROL FLIGHT CONF.; ANAHEIM, CALIF.; 1974; NEW YORK; AIAA; DA. 1974; VOL. 885; PP. 1-7; BIBL. 20 REF.Conference Paper

A STUDY ON AIRCRAFT MAP DISPLAY LOCATION AND ORIENTATION.BATY DL; WEMPE TE; HUFF EM et al.1974; I.E.E.E. TRANS. SYST. MAN CYBERN.; U.S.A.; DA. 1974; VOL. 4; NO 6; PP. 560-568; BIBL. 4 REF.Article

PRACTICAL OPTIMAL FLIGHT CONTROL FOR AIRCRAFT WITH LARGE FLIGHT ENVELOPESVANDIERENDONCK AJ.sdIN: AIAA 11TH AEROSP. SCI. MEET.; WASHINGTON; 1973; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 159; PP. 1-6; BIBL. 8 REF.Conference Paper

AUSLEGUNG VON FLUGREGLERN MIT HILFE MODERNER SYSTEMTHEORIE. = CONSTRUCTION DE SYSTEMES DE CONTROLES DU VOL A L'AIDE DE LA THEORIE MODERNE DES SYSTEMESSCHANZER G.1975; Z. FLUGWISSENSCH.; DTSCH.; DA. 1975; VOL. 23; NO 4; PP. 129-137; ABS. ANGL. FR.; BIBL. 16 REF.Article

PILOT/AUTOMATIC-RELATIONS, CONFIDENCE, DISPLAYS = RELATIONS PILOTE/SYSTEME AUTOMATIQUE; CONFIANCE ET VISUALISATIONWILCKENS V.1973; SOC. EXPER. TEST PILOTS, TECH. REV.; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 72-86; BIBL. 10 REF.Serial Issue

DEVELOPMENTS IN AIRCRAFT DIGITAL SYSTEMS = DEVELOPPEMENTS DANS LES SYSTEMES NUMERIQUES POUR L'AERONAUTIQUERUGGLES R; SCOTT EM.1973; A.G.A.R.D. CONF. PROC.; FR.; DA. 1973; NO 114; PP. 19.1-19.11; (24TH TECH. MEET. AVIONICS PANEL AGARD: AUTOM. MANNED AEROSP. SYST.; DAYTON, OHIO; 1972)Conference Paper

SOME EFFECTS OF BIAS ERRORS IN REDUNDANT FLIGHT CONTROL SYSTEMS = QUELQUES EFFETS D'ERREURS DE BIAIS DANS DES SYSTEMES DE COMMANDE DE VOL REDONDANTSSTENGEL RF.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 150-156; BIBL. 3 REF.Serial Issue

BELL COMMERCIAL AUTOMATIC FLIGHT CONTROL SYSTEM DESIGN AND TEST = CONCEPTION ET ESSAIS DU SYSTEME COMMERCIAL BELL DE COMMANDE AUTOMATIQUE DE VOLERHART RG.1973; SOC. EXPER. TEST PILOTS, TECH. REV.; U.S.A.; DA. 1973; VOL. 11; NO 3; PP. 58-61Serial Issue

DIGITAL FILTERS FOR FLIGHT CONTROL.1973; IN: 14TH JT. AUTOM. CONTROL CONF. AM. AUTOM. CONTROL COUNC.; COLUMBUS, OHIO; 1973; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1973; PP. 49-60; BIBL. DISSEM.Conference Paper

THE APPLICATION OF A MODAL DAMPING CONSTRAINT IN CONJUNCTION WITH THE OPTIMISATION OF TIME RESPONSES TO THE DESIGN OF FLIGHT CONTROL SYSTEMSBURT PJ.1973; I.E.E. CONF. PUBL.; G.B.; DA. 1973; NO 96; PP. 19-28; BIBL. 1 P.; (CONF. COMPUT. AIDED CONTROL SYST. DES.; CAMBRIDGE; 1973)Conference Paper

Towards more resilient flight controlLOMBAERTS, Thomas; SMAILI, Hafid; BREEMAN, Jan et al.Fault tolerant flight control (a benchmark challenge). Lecture notes in control and information sciences. 2010, Vol 399, pp 3-45, issn 0170-8643, isbn 978-3-642-11689-6 3-642-11689-2, 1Vol, 43 p.Book Chapter

Flight control century: Triumphs of the systems approachMCRUER, Duane; GRAHAM, Dunstan.Journal of guidance, control, and dynamics. 2004, Vol 27, Num 2, pp 161-173, issn 0731-5090, 13 p.Article

MINIMUM FUEL ROCKET MANEUVERS IN HORIZONTAL FLIGHT = MANOEUVRE DE FUSEE A CONSOMMATION MINIMALE DE COMBUSTIBLE EN VOL HORIZONTALVINH NX.1973; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 2; PP. 165-169; BIBL. 2 REF.Serial Issue

MODIFICATIONS SINCE CONCORDE 0011973; AIRER. ENGNG; G.B.; DA. 1973; VOL. 45; NO 4; PP. 4-26 (20 P.)Serial Issue

Multiparadigm design, validation and verification by simulation in flight control system developmentLIU, Hugh H. T.IEEE International Symposium on computer aided control systems design. 2004, pp 71-76, isbn 0-7803-8636-1, 1Vol, 6 p.Conference Paper

Advances techniques for clearance of flight control lawsFielding, Christopher; Varga, Andras; Bennani, Samir et al.Lecture notes in control and information sciences. 2002, issn 0170-8643, isbn 3-540-44054-2, IX, 469 p, isbn 3-540-44054-2Book

Synthetic-Waypoint Guidance Algorithm for Following a Desired Flight TrajectoryMEDAGODA, Eran D. B; GIBBENS, Peter W.Journal of guidance, control, and dynamics. 2010, Vol 33, Num 2, pp 601-606, issn 0731-5090, 6 p.Article

Flight Control Software: Mistakes Made and Lessons Learned : SAFETY-CRITICAL SOFTWAREJEPPU, Yogananda.IEEE software. 2013, Vol 30, Num 3, pp 67-72, issn 0740-7459, 6 p.Article

Constrained Linear Quadratic Tracker for Optimal Flight PerformanceDE ALMEIDA, Fabio A; GUERRA, Eduardo Bento; D'OLIVEIRA, Flavio Araripe et al.Journal of guidance, control, and dynamics. 2012, Vol 35, Num 6, pp 1911-1918, issn 0731-5090, 8 p.Article

Fuel-Efficient Formation Flight-Control Design Based on Energy ManeuverabilityCHOI, Jongug; KIM, Youdan.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 4, pp 1145-1150, issn 0731-5090, 6 p.Article

Full-envelope robust control of a shrouded-fan unmanned vehicleAVANZINI, Giulio; CINIGLIO, Umberto; DE MATTEIS, Guido et al.Journal of guidance, control, and dynamics. 2006, Vol 29, Num 2, pp 435-443, issn 0731-5090, 9 p.Article

RECOVER: A Benchmark for Integrated Fault Tolerant Flight Control EvaluationSMAILI, Hafid; BREEMAN, Jan; LOMBAERTS, Thomas et al.Fault tolerant flight control (a benchmark challenge). Lecture notes in control and information sciences. 2010, Vol 399, pp 171-221, issn 0170-8643, isbn 978-3-642-11689-6 3-642-11689-2, 1Vol, 51 p.Book Chapter