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ASYMPTOTIC SOLUTION TO THE PROBLEM OF OPTIMAL LOW-THRUST ENERGY INCREASE = SOLUTION ASYMPTOTIQUE POUR LE PROBLEME DE L'ACCROISSEMENT OPTIMAL DE L'ENERGIE A FAIBLE POUSSEEJACOBSON RA; POWERS WF.1972; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1972; VOL. 10; NO 12; PP. 1679-1680; BIBL. 6 REF.Serial Issue

ZUR INTEGRATION REGULARISIERTER BEWEGUNGSGLEICHUNGEN VON SATELLITENAUFSTIEGSBAHNEN = INTEGRATION DES EQUATIONS REGULARISEES DU MOUVEMENT SUR LES TRAJECTOIRES ASCENSIONNELLES DES SATELLITESHENSCHEL F.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 2; PP. 68-72; BIBL. 1 REF.Serial Issue

OPTIMAL TRAJECTORIES BETWEEN EARTH AND MARS IN THEIR TRUE PLANETARY ORBITSGRAVIER JP; MARCHAL C; CULP RD et al.1972; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1972; VOL. 9; NO 2; PP. 120-136; BIBL. 3 REF.Serial Issue

HYPERBOLIC ORBIT EQUATIONS WITH ASYMPTOTE-BASED COORDINATES = EQUATIONS POUR ORBITES HYPERBOLIQUES UTILISANT LES ASYMPTOTES COMME AXES DE COORDONNEESMCDERMOTT AM.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 5-6Serial Issue

GENERAL THEORY OF OPTIMAL TRAJECTORY FOR ROCKET FLIGHT IN A RESISTING MEDIUMVINH NX.1973; J. OPTIMIZ. THEORY APPL.; U.S.A; DA. 1973; VOL. 11; NO 2; PP. 189-202; BIBL. 9 REF.Serial Issue

OPTIMAL PURSUIT IN SPACE = TRAJECTOIRE OPTIMALE DE POURSUITE DANS L'ESPACEHAMZA MH; SALAMA AIA.1973; Z. FLUGWISSENSCH.; DTSCH.; DA. 1973; VOL. 21; NO 5; PP. 173-178; ABS. ALLEM. FR.; BIBL. 6 REF.Serial Issue

INTEGRALS OF THE MOTION FOR OPTIMAL TRAJECTORIES IN ATMOSPHERIC FLIGHT = INTEGRALES DU MOUVEMENT POUR LES TRAJECTOIRES OPTIMALES DU VOL ATMOSPHERIQUEVINH NX.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 700-703; BIBL. 9 REF.Serial Issue

STRATEGIES FOR CONTROL OF THE SPACE SHUTTLE TRANSITION = STRATEGIES DE COMMANDE DE LA TRANSITION DE LA NAVETTE SPATIALESTENGEL RF.1973; J. SPACECR. ROCK.; U.S.A.; DA. 1973; VOL. 10; NO 1; PP. 77-84; BIBL. 14 REF.Serial Issue

POWERED-FLIGHT TRAJECTORY OPTIMIZATION FOR AN INERTIAL-GUIDANCE BALLISTIC VEHICLE = OPTIMISATION DE LA TRAJECTOIRE DE VOL PROPULSE D'UN VEHICULE BALISTIQUE A GUIDAGE INERTIELHOY EC; LEONDES CT.1972; ASTRONAUT. ACTA; G.B.; DA. 1972; VOL. 17; NO 6; PP. 857-870; ABS. FR. ALLEM.; BIBL. 3 REF.Serial Issue

RENDEZVOUS PROBLEM = PROBLEMES DE RENDEZ-VOUSHOUBOLT JC.1966; IN: SPACE MATH. PROC. SUMMER SEMIN. ITHACA, N.Y., 1963; PROVIDENCE, R.I.; AM. MATH. SOC.; DA. 1966; PP. 276-301Conference Proceedings

INTEGRATION OF THE PRIMER VECTOR IN A CENTRAL FORCE FIELDVINH NX.1972; J. OPTIMIZ. THEORY APPL.; U.S.A.; DA. 1972; VOL. 9; NO 1; PP. 51-58; BIBL. 7 REF.Serial Issue

FAILURE OF A SELF-CONSISTENT DIFFRACTIVE MULTIPERIPHERAL MODEL IN THE STRONG-ORDERING LIMITJONES ST.1973; PHYS. REV., D; U.S.A.; DA. 1973; VOL. 7; NO 1; PP. 197-201; BIBL. 11 REF.Serial Issue

DERIVEES ISOCHRONES PAR RAPPORT A CERTAINS PARAMETRES DE LA TRAJECTOIRE D'UN SPATIONEFBAKHSHIYAN B TS.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 2; PP. 217-225; BIBL. 5 REF.Serial Issue

QUELQUES PROBLEMES SUR LA DIRECTION OPTIMALE DE LA TRAJECTOIRE D'UN SPATIONEF DANS L'ATMOSPHERE DE MARSIVANOV NM; MARTYNOV AI; SHILOV AA et al.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 1; PP. 21-30; BIBL. 4 REF.Serial Issue

SINGLET BOSON TRAJECTORYPEASLEE DC.1972; PHYS. REV. LETTERS; U.S.A.; DA. 1972; VOL. 29; NO 23; PP. 1573-1575; BIBL. DISSEM.Serial Issue

CORRECTION DE TRAJECTOIRE D'UN SPATIONEF COMPORTANT UNE CABINE FIXE DU MOTEUR DE CORRECTIONBORZOV VI.1972; VEST. MOSKOV. UNIV. 1; S.S.S.R.; DA. 1972; NO 6; PP. 93-100; ABS. ANGL.; BIBL. 5 REF.Serial Issue

ACCELERATING ONE-DIMENSIONAL SEARCHES = AMELIORATION DE LA RAPIDITE DES RECHERCHES UNIDIMENSIONNELLESJOHNSON IL JR; KAMM JL.1973; A.I.A.A.J., NEW YORK; U.S.A.; DA. 1973; VOL. 11; NO 5; PP. 757-759; BIBL. 10 REF.Serial Issue

ESTIMATING TRAJECTORY CORRECTION REQUIREMENTS FOR MULTIPLE OUTER PLANET MISSIONSFRIEDMAN LD; HAMILTON TW; STANTON RH et al.1972; J. SPACECR. ROCK.; U.S.A.; DA. 1972; VOL. 9; NO 12; PP. 909-914; BIBL. 10 REF.Serial Issue

EIN VERFAHREN ZUR BERECHNUNG VON EBENEN UBERGAENGEN IM NEWTONSCHEN ZENTRALKRAFTFELD = METHODE DE CALCUL DU TRANSFERT COPLANAIRE DANS UN CHAMP DE FORCES CENTRALES NEWTONIENSOMMER H.1973; DTSCHE LUFT-U. RAUMFAHRT, FORSCH.-BER.; DTSCH.; DA. 1973; NO 29; PP. 1-45; ABS. ANGL.; BIBL. 2 P.Serial Issue

ON-OFF AND ACCELERATION CONTROL OF SOLID ROCKETSMCDONALD AJ.1971; S.A.E. TRANS.; U.S.A.; DA. 1971; VOL. 80; NO PART 4; PP. 2576-2585; BIBL. 27 REF.Serial Issue

THE EFFECTS OF TRAJECTORY CHARACTERISTICS ON SCIENTIFIC OBJECTIVES FOR MAJOR PLANETARY ORBITERSPAUL CK.1972; J. ASTRONAUT. SCI.; U.S.A.; DA. 1972; VOL. 20; NO 2; PP. 65-87; BIBL. 8 REF.Serial Issue

ALGORITHME A GRADIENT AVEC SUPERMEMOIRE ET RESTITUTION DONNEES DANS LES PROBLEMES D'OPTIMISATION D'UNE TRAJECTOIRE DE VOLTALYZIN VA.1972; IZVEST. VYSSH. UCHEBN. ZAVED., AVIAC. TEKH.; S.S.S.R.; DA. 1972; NO 4; PP. 39-45; BIBL. 3 REF.Serial Issue

SOLVING FLIGHT-PATH OPTIMIZATION PROBLEMS ON A MINICOMPUTER = RESOLUTION PAR ORDINATEUR DES PROBLEMES D'OPTIMISATION DES TRAJECTOIRES DE VOLTHOMASSON FY; COOK G.1973; ASTRONAUT. ACTA; G.B.; DA. 1973; VOL. 18; NO 1; PP. 45-51; ABS. ALLEM. FR.; BIBL. 1 REF.Serial Issue

PD-, DD- SCATTERING AND POMERON TRAJECTORYILYIN VV; JENKOVSZKY LL; TUTIK RS et al.1972; ITF-72-152E; U.S.S.R.; DA. 1972; PP. (7 P.); BIBL. 15 REF.Report

SUR LE PROBLEME RELATIF A UNE FAMILLE DE TRAJECTOIRES NON PARALLELES DE REGGEKOLOMYTSEV VI.1972; TEOR. MAT. FIZ.; S.S.S.R.; DA. 1972; VOL. 12; NO 1; PP. 40-47; ABS. ANGL.; BIBL. 13 REF.Serial Issue

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