Ilia S. Grigoriev
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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
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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
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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
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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
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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
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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
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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)
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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)
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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
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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
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I.S. Grigoriev and M.P. Zapletin
About one problem of trajectory optimization
Cosmic Research, 2008, vol. 46, No. 3.
Abstract
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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
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Cosmic Research (Kosmicheskie Issledovaniya)
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