Simple Real-Time Stabilization of Vertical Takeoff and Landing Aircraft with Bounded SignalsSANCHEZ, A; GARCIA, P; CASTILLO, P et al.Journal of guidance, control, and dynamics. 2008, Vol 31, Num 4, pp 1166-1176, issn 0731-5090, 11 p.Article

Review of multivariable control applied to the VAAC Harrier and remaining open questionsHYDE, Rick A.Lecture notes in control and information sciences. 2006, pp 183-202, issn 0170-8643, isbn 3-540-31754-6, 1Vol, 20 p.Conference Paper

CASA 212 AVIOCAR1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 4; PP. 355Serial Issue

HARRIER ON THE GUAM. A BLUEPRINT FOR THE 1970'SSMITH LA.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 853; PP. 1-14Conference Paper

COMPARISON OF PROPULSION SYSTEM CONCEPTS FOR V/STOL COMMERCIAL TRANSPORTSZABINSKY JM; CARTER RN.sdIN: AM. INST. AERONAUT. ASTRONAUT. SOC. AUTOMOT. ENG. 8TH. JOINT PROPUL. SPEC. CONF.; NEW ORLEANS, LA.; 1972; NEW YORK; A.I.A.A.; DA. S.D.; NO 1176; PP. 1-11; BIBL. 5 REF.Conference Paper

ANTHROPOTECHNISCHE UNTERSUCHUNG EINER UBERGRUNDANZEIGE UND EINES KUENSTLICHEN HORIZONTS MIT VORANZEIGE ZUR MANUELLEN REGELUNG VON VTOL-FLUGZEUGEN = RECHERCHES ANTHROPOTECHNIQUES SUR UNE VISUALISATION DU SOL ET UN HORIZON ARTIFICIEL AVEC INFORMATION PREVISIONNELLE POUR LE REGLAGE MANUEL D'ATTITUDE DES AVIONS ADAVDEY D; JOHANNSEN G.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 4; PP. 140-145; ABS. ANGL. FR.; BIBL. 10 REF.Serial Issue

PREDICTION METHODS FOR JET V/STOL PROPULSION AERODYNAMICS.PLATZER MF; MARGASON RJ.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 69-77; BIBL. 1 P. 1/2Article

LE HS.146. UN NOUVEAU CONCURRENT SUR ETAPES COURTES1973; INTERAVIA; SUISSE; DA. 1973; VOL. 28; NO 8; PP. 887-888Serial Issue

ATC SYSTEM PLANNING FOR V*STOL AVIATIONRICHARDSON RA.1973; I.E.E.E. TRANS. COMMUNIC.; U.S.A.; DA. 1973; VOL. 21; NO 5; PP. 529-531Serial Issue

DIE BEDEUTUNG DER AERODYNAMISCHEN STRAHL-INTERFERENZ BEI DER ENTWICKLUNG UND ERPROBUNG DES V/STOL-TRANSPORTFLUGZEUGES DO 31 = LA SIGNIFICATION DE L'INTERFERENCE DANS LA REACTION AERODYNAMIQUE, LE DEVELOPPEMENT ET LE CONTROLE DE L'APPAREIL DE TRANSPORT ADAC/V DO 31WELTE D.sdIN: 5. JAHRESTAG. DTSCH. GES. LUFT RAUMFAHRT; BERLIN; 1972; S.L.; DA. S.D.; PP. 1-14; H.T. 10; BIBL. 2 REF.Conference Paper

On (civil) aviation future(s)BUSHNELL, D. M.Aeronautical Journal. 2001, Vol 105, Num 1052, pp 603-606, issn 0001-9240Article

DREIKOMPONENTENMESSUNGEN AM MODELL EINES LEICHTEN STOL-FLUGZEUGS MIT AUSBLASEN IN FLUEGELTIEFENRICHTUNG. = MESURES A TROIS COMPOSANTES SUR UNE MAQUETTE D'AVION LEGER DE TYPE ADAC AVEC SOUFFLAGE A L'INTERIEUR DE L'AILEKORNER H; LOHR R.1975; DTSCHE LUFT- U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1975; VOL. 75; NO 74; PP. 1-21; ABS. ANGL.; BIBL. 8 REF.Serial Issue

ADVANCED TECHNOLOGY FOR STOL TRANSPORTSCORNISH JJ III.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2497-2506Serial Issue

BENEFIT-COST ANALYSIS OF DELAY REDUCTION WITH STOLBARRIAGE JB; PRICE SPE.1973; PROC. AMER. SOC. CIV. ENGRS, TRANSPORT. ENGNG J. A.S.C.E.; U.S.A.; DA. 1973; VOL. 99; NO 1; PP. 43-52; BIBL. 11 REF.Serial Issue

NOISE RADIATION FROM V/STOL AIRCRAFTLOWSON MV.sdIN: 8TH CONGR. INT. COUNC. AERONAUT. SCI.; AMSTERDAM; 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 22; PP. 1-12; BIBL. 1 P.Conference Paper

A BASIC STUDY OF THE STOL GROUND EFFECT PROBLEM FOR PLANAR FLOW.KOTANSKY DR; BOWER WW.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 4; PP. 214-221; BIBL. 6 REF.Article

ZUR ENTWICKLUNG SENKRECHT STARTENDER FLUGZEUGE = DEVELOPPEMENT DES AVIONS ADAVKUNZLER M.1973; SCHWEIZ. BAUZTG; SCHWEIZ; DA. 1973; VOL. 91; NO 8; PP. 181-182Serial Issue

PREDICTION OF GROUND EFFECTS FOR VTOL AIRCRAFT WITH TWIN LIFTING JETS.LOUISSE J; MARSHALL F.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 2; PP. 123-127; BIBL. 14 REF.Article

L'AUGMENTATION DE POUSSEE DES TROMPES A JETS PULSANTS OU BATTANTS.DIDELLE H.1976; GRENOBLE; DA. 1976; PP. 1-249; BIBL. 4 P. 1/2; (THESE DOCT.-ING.; UNIV. SCI. MED. GRENOBLE)Thesis

LARGE WINDTUNNELS: REQUIRED CHARACTERISTICS AND THE PERFORMANCE OF VARIOUS TYPES OF TRANSONIC FACILITY.PANKHURST RC.1974; AGARD-R-615; FR.; DA. 1974; PP. (155P.); ABS. ANGL.; BIBL. DISSEM.Report

CHOICES FOR THE FUTURE: AN INDUSTRY VIEWPOINT ON PROTOTYPING = CHOIX POUR LE FUTUR: POINT DE VUE DE L'INDUSTRIE SUR L'UTILISATION DES PROTOTYPESALTIS HD.1972; IN: SOC. AUTOMOT. ENG. NATL. AEROSP. ENG. MANUF. MEET.; SAN DIEGO, CALIF.; 1972; NEW YORK; SOC. AUTOMOT. ENG.; DA. 1972; VOL. 848; PP. 1-6Conference Paper

FORWARD FLIGHT EFFECTS ON MIXER NOZZLE DESIGN AND NOISE CONSIDERATIONS FOR STOL EXTERNALLY BLOWN FLAP SYSTEMS = EFFETS DU VOL EN TRANSLATION SUR LA CONCEPTION D'UNE TUYERE A MELANGEUR ET CONSIDERATIONS DE BRUIT POUR LES SYSTEMES DE VOLETS SOUFFLES DE L'EXTERIEUR D'AVION ADACVON GLAHN U; SEKAS N; GROESBECK D et al.sdIN: AIAA 4TH AIRCR. DES. FLIGHT TEST OPER. MEET. LOS ANGELES, 1972; NEW YORK; AM. INST. AERONAUT. ASTRONAUT.; DA. S.D.; VOL. 792; PP. 1-8; BIBL. 9 REF.Conference Paper

GROUND EFFECTS ON LIFT FOR TURBOFAN POWERED-LIFT STOL AIRCRAFT.CAMPBELL JP; HASSEL JL JR; THOMAS JL et al.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 78-84; BIBL. 27 REF.Article

DEVELOPMENT OF THEORETICAL MODELS FOR JET-INDUCED EFFECTS ON V/STOL AIRCRAFT.SICLARI MJ; MIGDAL D; LUZZI TW JR et al.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 12; PP. 938-944; BIBL. 12 REF.Article

DETERMINING STOL RIDE QUALITY CRITERIA-PASSENGER ACCEPTANCE = DETERMINATION DE L'ACCEPTATION PAR LES PASSAGERS DES CRITERES DE QUALITE DE VOL DES ADACJACOBSON ID; KUHLTHAU AR.1973; J. AIRCR.; U.S.A.; DA. 1973; VOL. 10; NO 3; PP. 163-166; BIBL. 6 REF.Serial Issue