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 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

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 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

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

Trajectory-based-presentation of heterogeneous spatio-temporal contentTEZUKA, Taro; TANAKA, Katsumi.Lecture notes in computer science. 2005, pp 235-245, issn 0302-9743, isbn 3-540-30848-2, 1Vol, 11 p.Conference Paper

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

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

On periodic billiard trajectories in obtuse trianglesHALBEISEN, Lorenz; HUNGERBÜHLER, Norbert.SIAM review (Print). 2000, Vol 42, Num 4, pp 657-670, issn 0036-1445Article

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

Minimum-time path planning for robot arms and their dynamicsBYUNG KOOK KIM; SHIN, K. G.IEEE transactions on systems, man, and cybernetics. 1985, Vol 15, Num 2, pp 213-223, issn 0018-9472Article

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

On singular extremals in the time minimal control problem in R³BONNARD, B.SIAM journal on control and optimization. 1985, Vol 23, Num 5, pp 794-802, issn 0363-0129Article

Target path controllability of linear time-varying dynamical systemsWOHLTMANN, H.-W.IEEE transactions on automatic control. 1985, Vol 30, Num 1, pp 84-87, issn 0018-9286Article

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

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

On the helical nature of neutral trajectories in the oceanMCDOUGALL, T. J; JACKETT, D. R.Progress in oceanography. 1988, Vol 20, Num 3, pp 153-183, issn 0079-6611Article