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MAXIMUM ALTITUDE SAILPLANE WINCH-LAUNCH TRAJECTORIES.PIERSON BL.1977; AERONAUT. QUART.; G.B.; DA. 1977; VOL. 28; NO 2; PP. 75-84; BIBL. 9 REF.Article

IMPROVED SECANT METHOD APPLIED TO BOOST TRAJECTORY OPTIMIZATION.GOTTLIEB RG; FOWLER WT.1977; J. SPACECR. ROCK.; U.S.A.; DA. 1977; VOL. 14; NO 2; PP. 96-101; BIBL. 17 REF.Article

OPTIMIZATION OF MISSILE TRAJECTOIRES BY MEANS OF EVOLUTION STRATEGYGAIDOSCH H.1980; AEROSPACE SCIENCES MEETING. 18/1980/PASADENA CA; USA; NEW YORK: AIAA; DA. 1980; 10 P.; BIBL. 2 REF.Conference Paper

OPTIMAL N-IMPULSE TRANSFER TRAJECTORIES USING KUSTAANHEIMO/STIEFEL VARIABLES.JEZEWSKI DJ.1977; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 3; PP. 390-394; BIBL. 5 REF.Article

MINIMUM-TIME RESCUE TRAJECTOIRES BETWEEN SPACECRAFT IN CIRCULAR ORBITS.HOLADAY BH; SWAIM RL.1976; J. SPACECR. ROCK.; U.S.A.; DA. 1976; VOL. 13; NO 7; PP. 393-399; BIBL. 12 REF.Article

MINIMUM-TIME 180O TURNS OF AIRCRAFT = VIRAGES DE 180O D'UN AVION EN TEMPS MINIMUMWELL KH; BERGER E.1982; J. OPTIM. THEORY APPL.; ISSN 0022-3239; USA; DA. 1982; VOL. 38; NO 1; PP. 83-96; BIBL. 8 REF.Article

OPTIMAL TWO-IMPULSE TRANSFER BETWEEN SPECIFIED TERMINAL STATES OF KEPLERIAN ORBITSJEZEWSKI DJ.1982; OPTIM. CONTROL APPL. METHODS; ISSN 0143-2087; GBR; DA. 1982; VOL. 3; NO 3; PP. 257; BIBL. 11 REF.Article

OPTIMALE TRAJEKTORIEN IM SPURYEBUNDENEN SCHNELLVERKEHR = TRAJECTOIRES OPTIMALES POUR DES SYSTEMES DE TRANSPORT RAPIDE SUR RAILKRAFT KH; SCHNIEDER E.1981; RT, REGELUNGSTECH.; ISSN 0340-434X; DEU; DA. 1981; VOL. 29; NO 5; PP. 152-155; BIBL. 10 REF.Article

ASTRODYNAMICS 1979PENZO P ED; KAUFMAN B ED; FRIEDMAN L ED et al.1979; ADV. ASTRONAUT. SCI.; USA; DA. 1979; VOL. 40; PART. 2; XVIII-481 P.; BIBL. DISSEM.Conference Paper

SHUTTLE ASCENT TRAJECTORY OPTIMIZATION WITH FUNCTION SPACE QUASI-NEWTON TECHNIQUES.EDGE ER; POWERS WF.1976; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1976; VOL. 14; NO 10; PP. 1369-1376; BIBL. 17 REF.Article

COMPUTER EFFICIENT DETERMINATION OF OPTIMUM PERFORMANCE ASCENT TRAJECTORIESFLEMING FW; KEMP VE.1982; J. ASTRONAUT. SCI.; ISSN 0021-9142; USA; DA. 1982; VOL. 30; NO 1; PP. 85-92Article

OPTIMAL NAVIGATION WITH RANDOM TERMINAL TIME IN THE PRESENCE OF PHASE CONSTRAINTSFRANKE J.1982; ZEITSCHRIFT FUER WAHRSCHEINLICHKEITSTHEORIE UND VERWANDTE GEBIETE; ISSN 0044-3719; DEU; DA. 1982; VOL. 60; NO 4; PP. 453-484; BIBL. 8 REF.Article

OPTIMALE TRAJEKTORIEN IM SPURGEBUNDENEN SCHNELLVERKEHR = TRAJECTOIRE OPTIMALE POUR DES SYSTEMES DE TRANSIT RAPIDE PAR RAILKRAFT KH; SCHNIEDER E.1981; RT, REGELUNGSTECH.; ISSN 0340-434X; DEU; DA. 1981; VOL. 29; NO 4; PP. 111-119; ABS. ENG; BIBL. 8 REF.Article

TECHNICAL NOTE ON THE NUMERICAL COMPUTATION OF MINIMUM-FUEL, EARTH-MARS TRANSFER.OBERLE HJ.1977; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1977; VOL. 22; NO 3; PP. 447-453; BIBL. 10 REF.Article

A NUMERICAL METHOD FOR GENERATING THREE-IMPULSE MINIMUM-TIME ORBITAL TRANSFERS.ANDERSON GM; BASINE JM.1977; J. ASTRONAUT. SCI.; U.S.A.; DA. 1977; VOL. 25; NO 2; PP. 107-121; BIBL. 10 REF.Article

FIXED-CHANGE OPTIMUM TRAJECTORIES FOR SHORT-HAUL AIRCRAFT.BARMAN JF; ERZBERGER H.1976; J. AIRCR.; U.S.A.; DA. 1976; VOL. 13; NO 10; PP. 748-754; BIBL. 10 REF.Article

OPTIMAL THREE-BURN ORBIT TRANSFER.BETTS JT.1977; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1977; VOL. 15; NO 6; PP. 861-864; BIBL. 5 REF.Article

TRAJECTORY OPTIMIZATION OF THE ATLAS/CENTAUR LAUNCH VEHICLE.BRUSCH RG.1976; IN: CONF. DECIS. CONTROL. SYMP. ADAPT. PROCESSES. 15. PROC.; CLEARWATER, FLA.; 1976; NEW YORK; INST. ELECTR. ELECTRON. ENG.; DA. 1976; PP. 492-500; BIBL. 1 P. 1/2Conference Paper

OPTIMAL TRAJECTORIES FOR THE DIVE-BOMBING MISSION OF A FIGHTER AIRCRAFT.PRASAD UR; SUBRAMANYAM PS.1977; J. AIRCR.; U.S.A.; DA. 1977; VOL. 14; NO 2; PP. 221-222; BIBL. 6 REF.Article

THE INTUITIVE DYNAMIC PROGRAMMING APPROACH TO OPTIMAL STOCHASTIC NAVIGATIONFRANKE J.1982; ZEITSCHRIFT FUER WAHRSCHEINLICHKEITSTHEORIE UND VERWANDTE GEBIETE; ISSN 0044-3719; DEU; DA. 1982; VOL. 60; NO 4; PP. 485-495; BIBL. 11 REF.Article

TIME-OPTIMAL CONTROL IN THE PLANESUSSMANN HJ.1982; LECT. NOTES CONTROL INF. SCI.; ISSN 0170-8643; DEU; DA. 1982; VOL. 39; PP. 244-260; BIBL. 2 REF.Conference Paper

PROPRIETES ASYMPTOTIQUES D'UNE CLASSE DE TRAJECTOIRES DE MODELES DEFINIS PAR DES CONES CONVEXESZHAFYAROV A ZH.1980; OPTIMIZACIJA; SUN; DA. 1980; NO 24; PP. 48-59; BIBL. 3 REF.Article

THEOREME DE LA TRAJECTOIRE AVEC UNE BORNE DE NEUMANN ET DES FONCTIONS D'OBJECTIF TERMINALE ET INTEGRALEALESHIN AV; SHMATKOV BA.1980; EKON. MAT. METODY; SUN; DA. 1980; VOL. 16; NO 1; PP. 194-198; BIBL. 3 REF.Article

CONJUGAISON DES PARTIES REGULIERES ET SINGULIERES DE LA COMMANDE OPTIMALEBERSHCHANSKIJ YA M.1979; AVTOMAT. I TELEMEKH.; SUN; DA. 1979; NO 3; PP. 5-11; ABS. ENG; BIBL. 8 REF.Article

TRAJECTOIRE DANS LA CONSOMMATION POUR UN MODELE DYNAMIQUE D'ECONOMIE EN TEMPS CONTINUDROZDOV NM.1979; AVTOMAT. I TELEMEKH.; SUN; DA. 1979; NO 10; PP. 65-69; ABS. ENG; BIBL. 4 REF.Article

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