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

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

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

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

SYNTHESIS OF THE TYPES OF OPTIMAL TRANSFERS BETWEEN HYPERBOLIC ASYMPTOTES. = SYNTHESE DES TYPES DE TRANSFERTS OPTIMAUX ENTRE DES ASYMPTOTES HYPERBOLIQUESWALTON JM; MARCHAL C; CULP RD et al.1975; A.I.A.A. J., NEW YORK; U.S.A.; DA. 1975; VOL. 13; NO 8; PP. 980-989; BIBL. 11 REF.Article

CONNECTION OF "PARABOLIC" MASS AND WIDTH TRAJECTORIES WITH HIGH-ENERGY SCATTERINGINGRAHAM RL.1972; PHYS. REV., D; U.S.A.; DA. 1972; VOL. 6; NO 1; PP. 329-335; BIBL. 35 REF.Serial Issue

A MODEL FOR THE POMERON TRAJECTORYCOHEN TANNOUDJI G; ILYIN VV; JENKOVSZKY LL et al.1972; LETTERE NUOVO CIMENTO; ITAL.; DA. 1972; VOL. 5; NO 14; PP. 957-962; BIBL. DISSEM.Serial Issue

LINEAR REGGE TRAJECTORIES AND HADRONIC LEVEL DEGENERACY AT HIGH ENERGIESSATZ H.1973; PHYS. LETTERS, B; NETHERL.; DA. 1973; VOL. 44; NO 4; PP. 373-376; BIBL. 14 REF.Serial Issue

TRANSFER MATRICES OF REAL R^-1 PRISMS WITH A SPIRAL MAIN PATH = MATRICES DE TRANSFERT DE PRESSES REELS EN R^-1 AVEC TRAJECTOIRE PRINCIPALE EN SPIRALEIOANOVICIU D.1973; INTERNATION. J. MASS. SPECTROM. ION PHYS.; NETHERL.; DA. 1973; VOL. 11; NO 2; PP. 185-195; BIBL. 4 REF.Serial Issue

DECOUPLING OF THE POMERANCHON REGGE TRAJECTORYBROWER RC; WEIS JH.1972; PHYS. LETTERS, B; NETHERL.; DA. 1972; VOL. 41; NO 5; PP. 631-634; BIBL. 10 REF.Serial Issue