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Optimal limited-rate slewing of a flexible spacecraft

International applied mechanics, 2010-09, Vol.46 (3), p.348-358

Zakrzhevskii, A. E.

2010

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Optimal slewing of a flexible spacecraft

International applied mechanics, 2003-10, Vol.39 (10), p.1208-1214

ZAKRZHEVSKII, A. E

2003

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Dynamics of spacecraft with gyro-gravitational system of stabilization due to elastic ring antenna deployment

Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science, 2011-10, Vol.225 (10), p.2333-2346

2011

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Method of Deployment of a Space Tethered System Aligned to the Local Vertical

The Journal of the astronautical sciences, 2016-09, Vol.63 (3), p.221-236

Zakrzhevskii, A. E.

2016

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Natural modes and frequencies of in-plane vibrations of a fixed elastic ring

International applied mechanics, 2011-05, Vol.46 (12), p.1420-1427

2011

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Modelling of Spacecraft Dynamics at Deployment of Large Elastic Structure

Modelling and Simulation in Engineering, 2012-01, Vol.2012, p.328-340

2012

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Dynamics of the orbital deployment of an elastic ring-shaped antenna

International applied mechanics, 2010-11, Vol.46 (6), p.718-729

2010

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Feed-Forward Control for Retrieval Mode of Space Tethered Systems

International Journal of Astronautics and Aeronautical Engineering, 2018-06, Vol.3 (1)

AE, Zakrzhevskii

2018

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Dynamics of a System of Bodies with Program-Variable Configuration

International applied mechanics, 2004-03, Vol.40 (3), p.345-350

2004

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Method of Deployment of a Tethered Space System Along the Local Vertical

International applied mechanics, 2015-11, Vol.51 (6), p.670-681

Zakrzhevskii, A. E.

2015

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The dynamics of systems of rigid and elastic bodies as applied to spacecraft

International applied mechanics, 2000-08, Vol.36 (8), p.1001-1036

ZAKRZHEVSKII, A. E

2000

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Stability analysis of gas pressure reducers of spacecraft

International applied mechanics, 2001-04, Vol.37 (4), p.544-549

2001

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Feed-forward control of total retrieval of the space tether from vertical position

Kosmìčna nauka ì tehnologìâ, 2021, Vol.27 (5), p.71-85

2021

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Motion parameters of an electrodynamic tether in orbit

International applied mechanics, 2007-03, Vol.43 (3), p.335-343

2007

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Deployment of reconfigurable spacecraft under earth conditions in the out-of-plane rotation mode

International applied mechanics, 2000-10, Vol.36 (10), p.1385-1392

2000

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On the dynamics of deployment of an orbital structure with elastic elements

International applied mechanics, 2006-08, Vol.42 (8), p.959-965

2006

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Dynamics of an Unstabilized Spacecraft During the Deployment of an Elastic Pantograph Structure

International applied mechanics, 2014-05, Vol.50 (3), p.341-351

2014

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Vertical displacement of an elastic container with a fluid

International applied mechanics, 1996-05, Vol.32 (5), p.389-394

ZAKRZHEVSKII, A. E

1996

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Analysis of errors in finite-dimensional modeling of the dynamics of a rigid body with elastic elements

International applied mechanics, 1994-07, Vol.30 (7), p.544-548

ZAKRZHEVSKII, A. E

1994

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Program motion of systems or rigid and elastic bodies (review)

International applied mechanics, 1993-06, Vol.29 (6), p.413-430

ZAKRZHEVSKII, A. E

1993

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Natural frequencies and modes of out-of-plane vibrations a fixed ring

International applied mechanics, 2011-12, Vol.47 (6), p.745-753

2011

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Expanding the flexible long element aboard spacecraft with the magnetic damper

Kosmìčna nauka ì tehnologìâ, 2014-01, Vol.20 (1(86)), p.28-43

2014

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Determination of a force transmitted by a plume of an ion thruster to an orbital object

Kosmìčna nauka ì tehnologìâ, 2016-01, Vol.22 (1(98)), p.52-63

2016

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The dynamics of the spacecraft with gyro-gravity stabilization in the deployment of a flexible ring antenna

Kosmìčna nauka ì tehnologìâ, 2011-09, Vol.17 (5), p.3-18

2011

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Spacecraft dynamics with regard to elastic gravitational stabilizer deployment

Acta astronautica, 2009-03, Vol.64 (5), p.501-513

2009

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Optimal limited-rate slewing of a flexible spacecraft

Optimal slewing of a flexible spacecraft

Dynamics of spacecraft with gyro-gravitational system of stabilization due to elastic ring antenna deployment

Method of Deployment of a Space Tethered System Aligned to the Local Vertical

Natural modes and frequencies of in-plane vibrations of a fixed elastic ring

Modelling of Spacecraft Dynamics at Deployment of Large Elastic Structure

Dynamics of the orbital deployment of an elastic ring-shaped antenna

Feed-Forward Control for Retrieval Mode of Space Tethered Systems

Dynamics of a System of Bodies with Program-Variable Configuration

Method of Deployment of a Tethered Space System Along the Local Vertical

The dynamics of systems of rigid and elastic bodies as applied to spacecraft

Stability analysis of gas pressure reducers of spacecraft

Feed-forward control of total retrieval of the space tether from vertical position

Motion parameters of an electrodynamic tether in orbit

Deployment of reconfigurable spacecraft under earth conditions in the out-of-plane rotation mode

On the dynamics of deployment of an orbital structure with elastic elements

Dynamics of an Unstabilized Spacecraft During the Deployment of an Elastic Pantograph Structure

Vertical displacement of an elastic container with a fluid

Analysis of errors in finite-dimensional modeling of the dynamics of a rigid body with elastic elements

Program motion of systems or rigid and elastic bodies (review)

Natural frequencies and modes of out-of-plane vibrations a fixed ring

Expanding the flexible long element aboard spacecraft with the magnetic damper

Determination of a force transmitted by a plume of an ion thruster to an orbital object

The dynamics of the spacecraft with gyro-gravity stabilization in the deployment of a flexible ring antenna

Spacecraft dynamics with regard to elastic gravitational stabilizer deployment

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