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Publications in Math-Net.Ru |
Citations |
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2020 |
| 1. |
V. V. Ivashkin, I. V. Krylov, “Optimization of trajectories for a spacecraft with an electric rocket engine of low thrust”, Keldysh Institute preprints, 2020, 094, 32 pp.  |
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2019 |
| 2. |
Peng Guo, V. V. Ivashkin, “An accuracy analysis for determining the orbits of hazardous asteroids by modeling the “Nebosvod” space system optical measurements”, Keldysh Institute preprints, 2019, 060, 32 pp.  |
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2018 |
| 3. |
P. Guo, V. V. Ivashkin, “Accuracy estimation for determining the motion parameters of a nonlinear dynamical system by the measurement result in the presence of interfering parameters”, Keldysh Institute preprints, 2018, 213, 36 pp. |
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| 4. |
P. Guo, V. V. Ivashkin, “Methods for calculating the gravitational potential of a homogeneous triaxial ellipsoid and their application to the analysis of asteroid's satellite dynamics”, Keldysh Institute preprints, 2018, 094, 32 pp. |
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| 5. |
V. V. Ivashkin, A. Lang, “Trajectory design for the Earth-asteroid-Earth mission taking into account the choice of the near-asteroid stay orbits”, Keldysh Institute preprints, 2018, 090, 27 pp. |
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2017 |
| 6. |
V. V. Ivashkin, A. Lang, “An analysis of optimality of trajectories for mission Earth–asteroid–Earth”, Keldysh Institute preprints, 2017, 113, 25 pp. |
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| 7. |
S. V. Belousov, V. V. Ivashkin, “Trajectories for flight to geostationary orbit using the gravitational field of the Moon”, Keldysh Institute preprints, 2017, 041, 36 pp. |
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2011 |
| 8. |
V. V. Ivashkin, I. V. Krylov, “Hybrid optimization method for space flight with low thrust and its use for flight from Earth to asteroid Apophis”, Keldysh Institute preprints, 2011, 056, 32 pp. |
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2008 |
| 9. |
V. V. Ivashkin, A. R. Golikov, ““Detour” trajectories for spacecraft flight between Earth and geostationary orbit using Moon's gravity”, Keldysh Institute preprints, 2008, 095, 24 pp. |
| 10. |
V. V. Ivashkin, V. G. Petukhov, “Trajectories for flight between Earth and Moon satellite orbits using intermediate orbit with capture by Moon”, Keldysh Institute preprints, 2008, 081, 32 pp. |
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2006 |
| 11. |
V. V. Ivashkin, “Trajectories for spacecraft return from geostationary orbit to the Earth using Moon's gravity”, Keldysh Institute preprints, 2006, 022, 20 pp. |
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2005 |
| 12. |
V. V. Ivashkin, “Ary Sternfeld and cosmonautics”, Keldysh Institute preprints, 2005, 020, 32 pp. |
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2003 |
| 13. |
V. V. Ivashkin, “Possible using analysis of laser influence on near-Earth object”, Keldysh Institute preprints, 2003, 089, 16 pp. |
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2001 |
| 14. |
V. V. Ivashkin, “On optimal trajectories of space flight to the Moon in the Earth-Moon-Sun system”, Keldysh Institute preprints, 2001, 085 |
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2000 |
| 15. |
Ph. I. Baum, V. V. Ivashkin, “Using Lunar Gravity Assist for Space Flight to Near - Earth Asteroid”, Keldysh Institute preprints, 2000, 067 |
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1999 |
| 16. |
Ph. I. Baum, V. V. Ivashkin, A. V. Chernov, “An Analysys of Spacecraft Optimal Two-Impulse Flights to Near-Earth Asteroid”, Keldysh Institute preprints, 1999, 034 |
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1998 |
| 17. |
V. V. Ivashkin, “A Model of Orbiting Spacecraft Motion near Cometary Nucleus. Part I”, Keldysh Institute preprints, 1998, 057 |
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1997 |
| 18. |
V. V. Ivashkin, A. V. Chernov, “Determination of Optimal Trajectories for the Space Mission to Near-Earth Asteroid with Using Low Thrust Engine”, Keldysh Institute preprints, 1997, 019 |
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1996 |
| 19. |
V. V. Zaytsev, V. V. Ivashkin, “Analysis of the Near-Earth Asteroid Obit Change Possibility by an Impact Kinetic Influence of the Spacecraft”, Keldysh Institute preprints, 1996, 070 |
| 20. |
V. V. Ivashkin, A. V. Chernov, “Optimal Trajectories Determination for Space Missions to Near-Earth Asteroid Using Low Thrust”, Keldysh Institute preprints, 1996, 062 |
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1990 |
| 21. |
V. V. Ivashkin, “Feasibility analysis of the autonomous optical navigation of a space probe for exploration of the Vesta asteroid”, Dokl. Akad. Nauk SSSR, 311:6 (1990), 1321–1324 |
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