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Results 1 to 25 of 53528

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CARACTERISTIQUES COMPAREES DE LA DISTRIBUTION DES DIMENSIONS DES PARTICULES DU SOL LUNAIRE AUX SITES D'ATTERRISSAGE DES SONDES "LUNA-16" ET "LUNA-20"STAKHEEV YU I; IVANOV AV; VUL'FSON EK et al.1976; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1976; VOL. 14; NO 3; PP. 428-434; BIBL. 19 REF.Article

THE AIRCRAFT LANDING TEST: AN INFORMATION PROCESSING APPROACH TO PILOT SELECTIONFOWLER B.1981; HUM. FACTORS; ISSN 0018-7208; USA; DA. 1981; VOL. 23; NO 2; PP. 129-137; BIBL. 27 REF.Article

A MODEL-BASED ANALYSIS OF A DISPLAY FOR HELICOPTER LANDING APPROACH.HESS RA; WHEAT LW.1976; I.E.E.E. TRANS. SYST. MAN CYBERN.; U.S.A.; DA. 1976; VOL. 6; NO 7; PP. 505-511; BIBL. 5 REF.Article

AIRCRAFT AUTOMATIC LANDINGMCDONALD JA.1980; NAVIGATION (WASHINGT.); ISSN 0028-1522; USA; DA. 1980; VOL. 27; NO 1; PP. 23-29Article

WIND MODELING AND LATERAL CONTROL FOR AUTOMATIC LANDING.HOLLEY WE; BRYSON AE JR.1977; J. SPACEER. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 2; PP. 65-72; BIBL. 27 REF.Article

THE ENVIRONS OF VIKING 2 LANDER.SHORTHILL RW; MOORE HJ II; HUTTON RE et al.1976; SCIENCE; U.S.A.; DA. 1976; VOL. 194; NO 4271; PP. 1309-1318; BIBL. 19 REF.Article

A JOINT PILOT-LANDING OFFICER SIMULATION PERFORMED TO DETERMINE AIRCRAFT WAVE-OFF PERFORMANCE REQUIREMENTS.NAVE RL.1976; A.G.A.R.D. CONF. PROC.; FR.; DA. 1976; NO 198; PP. 11.1-11.10; BIBL. 3 REF.; (FLIGHT SIMULATION-GUIDANCE SYST. SIMULATION. JT. FLIGHT MECH. PANEL-GUIDANCE CONTROL PANEL SYMP.; THE HAGUE; 1975)Conference Paper

APPLICATION OF FLIGHT SIMULATION TO DEVELOP, TEST, AND EVALUATE THE F-14A AUTOMATIC CARRIER LANDING SYSTEM.FORTENBAUGH RL; REBEL JM.1976; A.G.A.R.D. CONF. PROC.; FR.; DA. 1976; NO 198; PP. 5.1-5.13; BIBL. 4 REF.; (FLIGHT SIMULATION-GUIDANCE SYST. SIMULATION. JT. FLIGHT MECH. PANEL-GUIDANCE CONTROL PANEL SYMP.; THE HAGUE; 1975)Conference Paper

SURFACE EROSION CAUSED ON MARS FROM VIKING DESCENT ENGINE PLUMEHUTTON RE; MOORE HJ; SCOTT RF et al.1980; MOON AND PLANETS; ISSN 0165-0807; NLD; DA. 1980; VOL. 23; NO 3; PP. 293-305; BIBL. 9 REF.Article

ACTIVITE MOTRICE DU PILOTE AU COURS DE DIFFERENTS TYPES D'ATTERRISSAGEBRUSNICHKINA RI.1980; KOSM. BIOL. AVIAKOSM. MED.; SUN; DA. 1980; VOL. 14; NO 4; PP. 45-48; ABS. ENG; BIBL. 7 REF.Article

ON THE TERMINAL LANDING OF UNPOWERED LIFTING VEHICLESGREWAL SS; HEDGCOXE PG; SCHNEIDER WP et al.1979; AUTOMAT. CONTROL THEORY APPL.; CAN; DA. 1979; VOL. 7; NO 2; PP. 40-45; BIBL. 6 REF.Article

THE BACKSIDE PARAMETER VIEWED FROM OPTIMAL CONTROL.KATO K; SATO K.1978; J. AIRCR.; U.S.A.; DA. 1978; VOL. 15; NO 2; PP. 67-68; BIBL. 8 REF.Article

DETECTION BY PILOTS OF SYSTEM FAILURES DURING INSTRUMENT LANDINGS.EPHRATH AR; CURRY RE.1977; I.E.E.E. TRANS. SYST. MAN CYBERN.; U.S.A.; DA. 1977; VOL. 7; NO 12; PP. 841-848; BIBL. 18 REF.Article

SIMULATION DER VERKEHRSBELASTUNG BEI ANFLUG- UND LANDESYSTEMEN MIT STATISTISCHER ABFRAGE. = SIMULATION DE LA CHARGE DE TRAFIC, DANS LE CAS DE SYSTEMES D'APPROCHE ET D'ATTERRISSAGE COMPORTANT DES INTERROGATIONS STATISTIQUESSKUPIN W; ULLRICH R.1977; FREQUENZ; DTSCH.; DA. 1977; VOL. 31; NO 8; PP. 246-253; ABS. ANGL.; BIBL. 4 REF.Article

THE INFLUENCE OF VISUAL EXPERIENCE AND DEGREE OF STYLIZATION ON HEIGHT AND DISTANCE JUDGEMENT IN AIRCRAFT APPROACH SCENES.DORFEL G.1976; A.G.A.R.D. CONF. PROC.; FR.; DA. 1976; NO 198; PP. 15.1-15.9; BIBL. 5 REF.; (FLIGHT SIMULATION-GUIDANCE SYST. SIMULATION. JT. FLIGHT MACH. PANEL-GUIDANCE CONTROL PANEL SYMP.; THE HAGUE; 1975)Conference Paper

PLANKTIC FORAMINIFERS FROM THE TUSCAHOMA SAND (UPPER PALEOCENE) OF SOUTHWEST ALABAMA = LES FORAMINIFERES PLANCTONIQUES DES SABLES DE TUSCAHOMA (PALEOCENE SUPERIEUR) SUD-OUEST DE L'ALABAMAMANCINI ERNEST A; OLIVER GARY EARL.1981; MICROPALEONTOLOGY; ISSN 0026-2803; USA; DA. 1981; VOL. 27; NO 2; PP. 204-225; BIBL. 52 REF.; 7 PLANCH. ; ILL.Article

IS THE LANDING RESPONSE OF THE HOUSEFLY (MUSCA) DRIVEN BY MOTION OF A FLOW FIELD.WEHRHAHN C; HAUSEN K; ZANKER J et al.1981; BIOL. CYBERN.; ISSN 0340-1200; DEU; DA. 1981; VOL. 41; NO 2; PP. 91-99; BIBL. 27 REF.Article

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

THE LANDING SIGNAL OFFICER: AUDITORY ASPECTSROBERTSON RM; MAXWELL DW; WILLIAMS CE et al.1982; AVIAT., SPACE, ENVIRON. MED.; ISSN 0095-6562; USA; DA. 1982; VOL. 53; NO 7; PP. 670-675; BIBL. 3 REF.Article

APPLICATION OF ENDFIRE ARRAYS AT CONTEMPORARY GLIDE-SLOPE PROBLEM SITESMCFARLAND RH.1981; IEEE TRANS. AEROSP. ELECTRON. SYST.; ISSN 0018-9251; USA; DA. 1981; VOL. 17; NO 2; PP. 261-270; BIBL. 18 REF.Article

GUIDANCE ACCURACY CONSIDERATIONS FOR THE MICROWAVE LANDING SYSTEM PRECISION DMEKELLY RJ; LABERGE EFC.1980; NAVIGATION (WASHINGT.); ISSN 0028-1522; USA; DA. 1980; VOL. 27; NO 1; PP. 1-22; BIBL. 29 REF.Article

NEW COMMUTATED DOPPLER MICROWAVE LANDING SYSTEMCONNOR FR.1980; ELECTRON. LETTERS; GBR; DA. 1980; VOL. 16; NO 10; PP. 365-366; BIBL. 2 REF.Article

SHUTTLE VEHICLE SAFETY ASSURANCE IN UNPOWERED LANDING THROUGH ADAPTIVE CONTROL.ZHEVNIN AA; TOLOKNOV VI; SHEVIAKOV OV et al.1977; J. ASTRONAUT. SCI.; U.S.A.; DA. 1977; VOL. 25; NO 2; PP. 143-149; BIBL. 5 REF.Article

TOUCHDOWN PERFORMANCE WITH A COMPUTER GRAPHICS NIGHT VISUAL ATTACHMENT.PALMER EA; CRONN FW.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 2; PP. 89-92; BIBL. 10 REF.Article

INTERVALLES DE PRISE DE LA MOYENNE POUR OBTENIR LES VALEURS "INSTANTANEES" DES GRANDEURS METEOROLOGIQUES EN VUE D'ASSURER L'ATTERRISSAGE D'UN AVIONBOKHANOV VE.1979; TRUDY GLAVN. GEOFIZ. OBS. A.I. VOEJKOVA, LENINGRAD; SUN; DA. 1979; NO 433; PP. 38-43; BIBL. 12 REF.Article

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