Ilia S. Grigoriev


Publications (Rus version)

  1. K.G. Grigoriev and I.S. Grigoriev
    Optimal Trajectories of Flights of a Spacecraft with Jet Engine of High Limited Thrust between an Orbits of Artifical Earth Satellites and Moon
    Cosmic Research, 1994, vol. 31, No. 6. Abstract
  2. K.G. Grigoriev and I.S. Grigoriev
    Optimal Trajectories for the Return of a Spacecraft with Jet Engine of High Limited Thrust from the Moon to Earth
    Cosmic Research, 1995, vol. 33, No. 5. Abstract
  3. K.G. Grigoriev and I.S. Grigoriev
    Optimum Spatial Trajectories for the Flight of a Spacecraft with a Large Limited Thrust Jet Engine Between Orbits of Artifical Satellites of the Earth and the Moon
    Cosmic Research, 1997, vol. 35, No 1, pp. 47-70. Abstract
  4. K.G. Grigoriev, I.S. Grigoriev and Yu. D. Petrikova
    The Fastest Maneuvers of a Spacecraft with a Jet Engine of a Large Limited Thrust in a Gravitational Field in a Vacuum
    Cosmic Research, 2000, vol. 38, No 2, pp. 160-181. Abstract
  5. K.G. Grigoriev and I.S. Grigoriev
    Solving Optimization Problems for the Flight Trajectories of a Spacecraft with a High-Thrust Jet Engine in Pulse Formulation for an Arbitrary Gravitational Field in a Vacuum
    Cosmic Research, 2002, vol. 40, No. 1, pp. 81-103. Abstract
  6. K.G. Grigoriev and I.S. Grigoriev
    Conditions of the Maximum Principle in the Problem of Optimal Control over an Aggregate of Dynamic Systems and Their Application to Solution of the Problems of Optimal Control of Spacecraft Motion,
    Cosmic Research, 2003, vol. 41, No. 3, pp. 285-309. Abstract
  7. S.Yu. Ryzhov and I.S. Grigoriev
    On Solving the Problems of Optimization of Trajectories of Many-Revolution Orbit Transfers of Spacecraft,
    Cosmic Research, 2006, vol. 44, No. 3, pp. 258-267. Abstract)
  8. I.S. Grigoriev, M.P. Zapletin and E.V. Zapletina
    First ACT global trajectory optimisation competition: Results found at Moscow State University.
    Acta Astronautica (2007), aa2906. (Abstract)
  9. I.S. Grigoriev and K.G. Grigoriev
    The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I
    Cosmic Research, 2007, vol. 45, No. 4, pp. 258-267. Abstract
  10. I.S. Grigoriev and K.G. Grigoriev
    The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: II
    Cosmic Research, 2007, vol. 45, No. 6. Abstract
  11. I.S. Grigoriev and M.P. Zapletin
    About one problem of trajectory optimization
    Cosmic Research, 2008, vol. 46, No. 3. Abstract
  12. I.S. Grigoriev and M.P. Zapletin
    Constructing Pontryagin extremals for the optimal control problem of asteroid fly-by
    Automation and Remote Control Volume 70, Number 9 (2009), 1499-1513

Links
All abstracts
Cosmic Research (Kosmicheskie Issledovaniya)

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