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THE TRANSITION FROM ELLIPTIC TO HYPERBOLIC ORBITS IN THE TWO-BODY PROBLEM BY SLOW LOSS OF MASSVAN DER LAAN L; VERHULST F.1972; CELEST. MECH.; NETHERL.; DA. 1972; VOL. 6; NO 3; PP. 343-351; BIBL. 4 REF.Serial Issue

LA MAGIA DE LAS ORBITAS ELIPTICAS.BERRONDO M; FLORES J; NOVARO O et al.1974; REV. MEX. FIS.; MEX.; DA. 1974; VOL. 23; SUPPL. ENSENANZA; PP. 13-26; ABS. ANGL.; BIBL. 4 REF.Article

Expansion theory for the elliptic motion of arbitrary eccentricity and semi-major axis. VII: Elliptic expansions in terms of the sectorial variables for the seventh and eighth categoriesMOHAMED ADEL SHARAF.Astrophysics and space science. 1985, Vol 112, Num 1, pp 51-68, issn 0004-640XArticle

UNE METHODE POUR DETERMINER L'ORBITE ELLIPTIQUE A PARTIR DE DEUX POSITIONS HELIOCENTRIQUESSIMOVLJEVICJ JL.1977; SRPSKA AKAD. NAUKA UMETN., GLAS, ODELJ., PRIRODNOMAT. NAUKA; JUGOSL.; DA. 1977; NO 41; PP. 39-50; ABS. ANGL.; BIBL. 6 REF.Article

UNE METHODE POUR DETERMINER LA PROXIMITE DES ORBITES DES CORPS CELESTESSIMOVLJEVICJ JL.1974; SRPSKA AKAD. NAUKA UMETN., GLAS, ODELJ. PRIRODNO-MAT. NAUKA; JUGOSL.; DA. 1974; NO 37; PP. 9-17; ABS. ANGL.; BIBL. 2 REF.Article

OSCILLATIONS PLANES NON LINEAIRES D'UN SATELLITE SUR UNE ORBITE ELLIPTIQUEDEMIN VG; SINGKH RB.1973; KOSM. ISSLEDOV.; S.S.S.R.; DA. 1973; VOL. 11; NO 2; PP. 192-197; BIBL. 3 REF.Serial Issue

EFFET RELATIVISTE DE LA VARIABILITE DE LA ROTATION DU PULSAR SUR L'ORBITE ELLIPTIQUEZEL'DOVICH YA B; SHAKURA NI.1975; PIS'MA ASTR. ZH.; S.S.S.R.; DA. 1975; VOL. 1; NO 11; PP. 19-22; ABS. ANGL.; BIBL. 4 REF.Article

Neutron stars in close binaries with elliptical component orbitsTUTUKOV, A. V.Astronomy reports. 2005, Vol 49, Num 12, pp 993-1000, issn 1063-7729, 8 p.Article

Expansion theory for the elliptic motion of arbitrary eccentricity and semi-major axis. VIII: Elliptic expansions in terms of the sectorial variables for the ninth, tenth, eleventh, and twelfth categoriesMOHAMED ADEL SHARAF.Astrophysics and space science. 1985, Vol 116, Num 2, pp 251-283, issn 0004-640XArticle

Laplace's problem in mathematical aspectSERAFIN, R. A.Celestial mechanics. 1984, Vol 33, Num 1, pp 71-84, issn 0008-8714Article

A propos des oscillations d'un satellite sur une orbite elliptiqueBUROV, A. A.Kosmičeskie issledovaniâ. 1984, Vol 22, Num 1, pp 133-134, issn 0023-4206Article

Escape from Elliptic Orbit Using Constant Radial ThrustMENGALI, Giovanni; QUARTA, Alessandro A.Journal of guidance, control, and dynamics. 2009, Vol 32, Num 3, pp 1018-1022, issn 0731-5090, 5 p.Article

Expansion theory for the elliptic motion of arbitrary eccentricity and semi-major axis. VI. Elliptic expansions in terms of the sectorial variables for the fifth and sixth categoriesMOHAMED ADEL SHARAF.Astrophysics and space science. 1984, Vol 104, Num 2, pp 267-284, issn 0004-640XArticle

Mouvements périodiques d'un satellite axisymétrique par rapport au centre de gravité sous l'action d'un moment gravitationnelSAZONOV, V. V; SIDORYUK, M. E.Izvestiâ Akademii nauk SSSR. Mehanika tverdogo tela. 1984, Num 3, pp 6-16, issn 0572-3299Article

Structure of the Circumbinary Envelopes of Young Binary Stars with Elliptical OrbitsSYTOV, A. Yu; KAIGORODOV, P. V; FATEEVA, A. M et al.Astronomy reports. 2011, Vol 55, Num 9, pp 793-800, issn 1063-7729, 8 p.Article

Modern view on Laplace's problemHURNIK, H; SEFARIN, R. A.Celestial mechanics. 1983, Vol 31, Num 1, pp 53-72, issn 0008-8714Article

Bounds on the solution to Kepler's equationSERAFIN, R. A.Celestial mechanics. 1986, Vol 38, Num 2, pp 111-121, issn 0008-8714Article

PROBLEMES DU PROJET DE LA PHOTOGRAPHIE DE LA SURFACE DE LA TERRE A PARTIR DE VAISSEAUX COSMIQUESNAZAROV ND.1975; IZVEST. VYSSH. UCHEBN. ZAVED., GEOD. AEROFOTOS' EMKA; S.S.S.R.; DA. 1975; NO 1; PP. 41-50; BIBL. 3 REF.Article

Orbite elliptique de l'astéroïde 1985 CQ1 et remarques théoriques = Elliptic orbit of asteroid 1985 CQ1 and theoretical considerationsDEBEHOGNE, H.Astronomy and astrophysics (Berlin. Print). 1987, Vol 172, Num 1-2, pp 342-344, issn 0004-6361Article

EFFET DES ERREURS D'OBSERVATIONS DANS LES CALCULS D'ORBITES ELLIPTIQUES PAR LA METHODE DE GAUSS-ENCKE, AVEC AMELIORATION PAR VARIATION DES DISTANCES GEOCENTRIQUES.DEBEHOGNE H; ZAPPALA V; VAGHI S et al.1976; ACAD. R. BELG., BULL. CL. SCI.; BELG.; DA. 1976; VOL. 62; NO 3; PP. 210-217; BIBL. 3 REF.Article

LES FAISCEAUX DE TRAJECTOIRES MONOENERGETIQUES DES CORPS DANS UN CHAMP DE FORCE INVERSEMENT PROPORTIONNEL AU CARRE DE LA DISTANCE AU CENTRE DE FORCEWRONSKI AS.1974; POST. ASTRONAUT., BIUL. NAUK.; POLSKA; DA. 1974; VOL. 7; NO 2-3; PP. 195-217; ABS. RUSSE ANGL; (KONF. NAUK. POL. TOW. ASTRONAUT. CZNEGO AUGUSTOWIE POSWIECONA WSPOLCZESNYM ZAGADNIENIOM ASTRONAUT.; AUGUSTOW; 1973)Conference Paper

EXPANSION THEORY FOR THE ELLIPTIC MOTION OF ARBITRARY ECCENTRICITY AND SEMI-MAJOR AXIS. IV. REGULARISATION APPROACH BY USING SECTORS INDEPENDENT VARIABLESMOHAMED ADEL SHARAF.1982; ASTROPHYS. SPACE SCI.; ISSN 0004-640X; NLD; DA. 1982; VOL. 84; NO 1; PP. 73-97; BIBL. 6 REF.Article

APPROXIMATE VALUES OF TOUE ANOMALIES OF QUASICOMPLANAR ASTEROIDS IN PROXIMITY.LAZOVIC J.1974; PUBL. DEPT., UNIV. BEOGRAD; YUGOSL.; DA. 1974; NO 5; PP. 85-93; BIBL. 5 REF.Article

PERIODIC SOLUTIONS OF THE THIRD SORT FOR RESTRICTED PROBLEM OF THREE BODIES AND THEIR STABILITY1973; CELEST. MECH.; NETHERL.; DA. 1973; VOL. 7; NO 2; PP. 156-176; BIBL. 1 REF.Serial Issue

EXPANSION THEORY FOR THE ELLIPTIC MOTION OF ARBITRARY ECCENTRICITY AND SEMI-MAJOR AXIS. III. ANALYTICAL AND COMPUTIONAL DEVELOPMENTS OF THE FUNCTIONS H1(M)(EPSILON ,THETA )=COS M(COS-1(1-EPSILON SIN2THETA )); H2(EPSILON ,XI ,THETA )=LOG(1-XI +XI EPSILON SIN2THETA ); H3(Q)(EPSILON ,XI ,THETA )=(1-XI +XI EPSILON SIN2THETA )QMOHAMED ADEL SHARAF.1982; ASTROPHYS. SPACE SCI.; ISSN 0004-640X; NLD; DA. 1982; VOL. 84; NO 1; PP. 53-71; BIBL. 2 REF.Article

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