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Table of contents of journal: *Celestial mechanics and dynamical astronomy

Results: 101-125/514
Periodic solutions for resonance 4/3: Application to the construction of an intermediary orbit for Hyperion's motion
Authors: Stellmacher, I
Citation: I. Stellmacher, Periodic solutions for resonance 4/3: Application to the construction of an intermediary orbit for Hyperion's motion, CEL MEC DYN, 75(3), 1999, pp. 185-200
Fast procedure solving universal Kepler's equation
Authors: Fukushima, T
Citation: T. Fukushima, Fast procedure solving universal Kepler's equation, CEL MEC DYN, 75(3), 1999, pp. 201-226
On the distance function between two Keplerian elliptic orbits
Authors: Kholshevnikov, KV Vassiliev, NN
Citation: Kv. Kholshevnikov et Nn. Vassiliev, On the distance function between two Keplerian elliptic orbits, CEL MEC DYN, 75(2), 1999, pp. 75-83
The determination of gravitational potential differences from satellite-to-satellite tracking
Authors: Jekeli, C
Citation: C. Jekeli, The determination of gravitational potential differences from satellite-to-satellite tracking, CEL MEC DYN, 75(2), 1999, pp. 85-101
Analytical and numerical results on the stability of a planetary precessional model
Authors: Della Penna, G
Citation: G. Della Penna, Analytical and numerical results on the stability of a planetary precessional model, CEL MEC DYN, 75(2), 1999, pp. 103-124
Analytical solution of the Kozai resonance and its application
Authors: Kinoshita, H Nakai, H
Citation: H. Kinoshita et H. Nakai, Analytical solution of the Kozai resonance and its application, CEL MEC DYN, 75(2), 1999, pp. 125-147
Extrapolation of symplectic integrators
Authors: Blanes, S Casas, F Ros, J
Citation: S. Blanes et al., Extrapolation of symplectic integrators, CEL MEC DYN, 75(2), 1999, pp. 149-161
Two-body problems with drag or thrust: Qualitative results
Authors: Diacu, F
Citation: F. Diacu, Two-body problems with drag or thrust: Qualitative results, CEL MEC DYN, 75(1), 1999, pp. 1-15
Keplerian periodic orbits in the isosceles problem
Authors: Alfaro, M Monleon, CC
Citation: M. Alfaro et Cc. Monleon, Keplerian periodic orbits in the isosceles problem, CEL MEC DYN, 75(1), 1999, pp. 17-27
Behaviour of a new type of Runge-Kutta methods when integrating satellite orbits
Authors: Gonzalez, AB Martin, P Lopez, DJ
Citation: Ab. Gonzalez et al., Behaviour of a new type of Runge-Kutta methods when integrating satellite orbits, CEL MEC DYN, 75(1), 1999, pp. 29-38
Tidal effects in the earth-moon system and the earth's rotation
Authors: Krasinsky, GA
Citation: Ga. Krasinsky, Tidal effects in the earth-moon system and the earth's rotation, CEL MEC DYN, 75(1), 1999, pp. 39-66
On linking coefficient of two Keplerian orbits
Authors: Kholshevnikov, KV Vassiliev, NN
Citation: Kv. Kholshevnikov et Nn. Vassiliev, On linking coefficient of two Keplerian orbits, CEL MEC DYN, 75(1), 1999, pp. 67-74
A tenth order symplectic Runge-Kutta-Nystrom method
Authors: Tsitouras, C
Citation: C. Tsitouras, A tenth order symplectic Runge-Kutta-Nystrom method, CEL MEC DYN, 74(4), 1999, pp. 223-230
Combinations of satellite crossovers to study orbit and residual errors inaltimetry
Authors: Klokocnik, J Wagner, CA
Citation: J. Klokocnik et Ca. Wagner, Combinations of satellite crossovers to study orbit and residual errors inaltimetry, CEL MEC DYN, 74(4), 1999, pp. 231-242
Diurnal and subdiurnal terms in RDAN97 series
Authors: Roosbeek, F
Citation: F. Roosbeek, Diurnal and subdiurnal terms in RDAN97 series, CEL MEC DYN, 74(4), 1999, pp. 243-252
Lunisolar apsidal resonances at low satellite orbits
Authors: Breiter, S
Citation: S. Breiter, Lunisolar apsidal resonances at low satellite orbits, CEL MEC DYN, 74(4), 1999, pp. 253-274
Efficient symplectic integration of satellite orbits
Authors: Mikkola, S
Citation: S. Mikkola, Efficient symplectic integration of satellite orbits, CEL MEC DYN, 74(4), 1999, pp. 275-285
Explicit symplectic algorithms for time-transformed hamiltonians
Authors: Mikkola, S Tanikawa, K
Citation: S. Mikkola et K. Tanikawa, Explicit symplectic algorithms for time-transformed hamiltonians, CEL MEC DYN, 74(4), 1999, pp. 287-295
On the classical expansion of the perturbing function in individual orbital elements
Authors: Tupikova, I Soffel, M Klioner, S
Citation: I. Tupikova et al., On the classical expansion of the perturbing function in individual orbital elements, CEL MEC DYN, 74(3), 1999, pp. 147-152
Improved nutation series for the non-rigid earth with a precise adjustmentof parameters with nonlinear dependence
Authors: Getino, J MartIn, P Farto, JM
Citation: J. Getino et al., Improved nutation series for the non-rigid earth with a precise adjustmentof parameters with nonlinear dependence, CEL MEC DYN, 74(3), 1999, pp. 153-162
A new solution to the Lagrange's case of the three-body problem
Authors: Pina, E
Citation: E. Pina, A new solution to the Lagrange's case of the three-body problem, CEL MEC DYN, 74(3), 1999, pp. 163-174
Poincare's methode nouvelle by skew composition
Authors: Deprit, E Deprit, A
Citation: E. Deprit et A. Deprit, Poincare's methode nouvelle by skew composition, CEL MEC DYN, 74(3), 1999, pp. 175-197
Potentials having two orthogonal families of curves as trajectories
Authors: Puel, F
Citation: F. Puel, Potentials having two orthogonal families of curves as trajectories, CEL MEC DYN, 74(3), 1999, pp. 199-210
Solvable cases of Szebehely's equation
Authors: Grigoriadou, S Bozis, G Elmabsout, B
Citation: S. Grigoriadou et al., Solvable cases of Szebehely's equation, CEL MEC DYN, 74(3), 1999, pp. 211-221
Orbital distribution arbitrarily close to the homothetic equilateral triple collision in the free-fall three-body problem with equal masses
Authors: Umehara, H Tanikawa, K
Citation: H. Umehara et K. Tanikawa, Orbital distribution arbitrarily close to the homothetic equilateral triple collision in the free-fall three-body problem with equal masses, CEL MEC DYN, 74(2), 1999, pp. 69-94
Risultati: << | 101-125 | 126-150 | 151-175 | 176-200 | >>