Ivashkin Vyacheslav Vasil'evich

Publications in Math-Net.Ru

1. Optimization of trajectories for a spacecraft with an electric rocket engine of low thrust
   
   Keldysh Institute preprints, 2020, 094, 32 pp.
2. 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.
3. 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.
4. 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.
5. 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.
6. An analysis of optimality of trajectories for mission Earth–asteroid–Earth
   
   Keldysh Institute preprints, 2017, 113, 25 pp.
7. Trajectories for flight to geostationary orbit using the gravitational field of the Moon
   
   Keldysh Institute preprints, 2017, 041, 36 pp.
8. 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.
9. “Detour” trajectories for spacecraft flight between Earth and geostationary orbit using Moon's gravity
   
   Keldysh Institute preprints, 2008, 095, 24 pp.
10. Trajectories for flight between Earth and Moon satellite orbits using intermediate orbit with capture by Moon
    
    Keldysh Institute preprints, 2008, 081, 32 pp.
11. Trajectories for spacecraft return from geostationary orbit to the Earth using Moon's gravity
    
    Keldysh Institute preprints, 2006, 022, 20 pp.
12. Ary Sternfeld and cosmonautics
    
    Keldysh Institute preprints, 2005, 020, 32 pp.
13. Possible using analysis of laser influence on near-Earth object
    
    Keldysh Institute preprints, 2003, 089, 16 pp.
14. On optimal trajectories of space flight to the Moon in the Earth-Moon-Sun system
    
    Keldysh Institute preprints, 2001, 085
15. Using Lunar Gravity Assist for Space Flight to Near - Earth Asteroid
    
    Keldysh Institute preprints, 2000, 067
16. An Analysys of Spacecraft Optimal Two-Impulse Flights to Near-Earth Asteroid
    
    Keldysh Institute preprints, 1999, 034
17. A Model of Orbiting Spacecraft Motion near Cometary Nucleus. Part I
    
    Keldysh Institute preprints, 1998, 057
18. Determination of Optimal Trajectories for the Space Mission to Near-Earth Asteroid with Using Low Thrust Engine
    
    Keldysh Institute preprints, 1997, 019
19. Analysis of the Near-Earth Asteroid Obit Change Possibility by an Impact Kinetic Influence of the Spacecraft
    
    Keldysh Institute preprints, 1996, 070
20. Optimal Trajectories Determination for Space Missions to Near-Earth Asteroid Using Low Thrust
    
    Keldysh Institute preprints, 1996, 062
21. 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