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A Comprehensive Software Verification Technology for Onboard Control Systems of Spacecraft

Automation and remote control, 2023-10, Vol.84 (10), p.1047-1054

2023

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Controlling a Linear MIMO System by a Measurement Vector Using Multilevel Decomposition

Journal of computer & systems sciences international, 2020-03, Vol.59 (2), p.151-160

2020

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Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles

Russian aeronautics, 2019, Vol.62 (1), p.22-31

2019

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Superfast Iterative Solvers for Linear Matrix Equations

Doklady. Mathematics, 2018-09, Vol.98 (2), p.444-447

2018

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Terminal synthesis of orbital orientation for a spacecraft

Journal of computer & systems sciences international, 2017-07, Vol.56 (4), p.721-737

2017

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Output control of the spectrum of a linear dynamic system in terms of the Van der Woude method

Doklady. Mathematics, 2017-09, Vol.96 (2), p.457-460

2017

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Circumlunar Spacecraft Navigation Using the Measurements from Global Navigation Satellite Systems GLONASS, GPS, Galileo and BeiDou

Gyroscopy and navigation (Online), 2019-10, Vol.10 (4), p.187-195

2019

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Modification of the Terminal Control Algorithm for Descent under “Magnified” Disturbances after Returning from the Moon

Cosmic research, 2020-03, Vol.58 (2), p.122-137

2020

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LMI-Based Criteria of Controllability and Observability for a Descriptor MIMO System

Journal of computer & systems sciences international, 2018, Vol.57 (1), p.18-24

2018

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Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution

Russian aeronautics, 2017, Vol.60 (1), p.64-73

2017

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Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity

Russian aeronautics, 2018-04, Vol.61 (2), p.201-211

2018

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Satellite Navigation of Lunar Orbiting Spacecraft and Objects on the Lunar Surface

Gyroscopy and navigation (Online), 2019, Vol.10 (2), p.54-61

2019

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Modification of the Terminal Control Algorithm for Descent from Near-Earth Orbit Applied to “Enhanced” Disturbances

Cosmic research, 2019-05, Vol.57 (3), p.176-187

2019

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Output control of the longitudinal motion of a flying vehicle

Journal of computer & systems sciences international, 2015-09, Vol.54 (5), p.825-837

2015

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Terminal control of the trajectory and rotational motion of an active spacecraft during a rendezvous with a passive spacecraft

Journal of computer & systems sciences international, 2016-05, Vol.55 (3), p.435-445

2016

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General analytical forms for the solution of the Sylvester and Lyapunov equations for continuous and discrete dynamic systems

Journal of computer & systems sciences international, 2017, Vol.56 (1), p.1-18

2017

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Attitude control algorithms for a descent vehicle returning from the moon

Journal of computer & systems sciences international, 2017-05, Vol.56 (3), p.483-491

2017

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Band formulas for calculating the numerator’s coefficients of the transfer function of a single-input system

Journal of computer & systems sciences international, 2016-11, Vol.55 (6), p.856-864

2016

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Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators

Journal of computer & systems sciences international, 2015-07, Vol.54 (4), p.621-628

2015

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Solvability conditions of problem of synthesizing proportional-integral control of a linear MIMO system

Journal of computer & systems sciences international, 2016-09, Vol.55 (5), p.821-831

2016

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Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: Analytical synthesis

Journal of computer & systems sciences international, 2015, Vol.54 (1), p.93-103

2015

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Modification of the exact pole placement method and its application for the control of spacecraft motion

Journal of computer & systems sciences international, 2013-03, Vol.52 (2), p.279-292

2013

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History of spacecraft control systems

Automation and remote control, 2013-03, Vol.74 (3), p.331-347

2013

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Synthesis of linear postcompensators for signal processing of nonlinear systems of a special form

Journal of computer & systems sciences international, 2016, Vol.55 (1), p.138-149

2016

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Output control of a spacecraft motion spectrum

Journal of computer & systems sciences international, 2014-07, Vol.53 (4), p.576-586

2014

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A Comprehensive Software Verification Technology for Onboard Control Systems of Spacecraft

Controlling a Linear MIMO System by a Measurement Vector Using Multilevel Decomposition

Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles

Superfast Iterative Solvers for Linear Matrix Equations

Terminal synthesis of orbital orientation for a spacecraft

Output control of the spectrum of a linear dynamic system in terms of the Van der Woude method

Circumlunar Spacecraft Navigation Using the Measurements from Global Navigation Satellite Systems GLONASS, GPS, Galileo and BeiDou

Modification of the Terminal Control Algorithm for Descent under “Magnified” Disturbances after Returning from the Moon

LMI-Based Criteria of Controllability and Observability for a Descriptor MIMO System

Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution

Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity

Satellite Navigation of Lunar Orbiting Spacecraft and Objects on the Lunar Surface

Modification of the Terminal Control Algorithm for Descent from Near-Earth Orbit Applied to “Enhanced” Disturbances

Output control of the longitudinal motion of a flying vehicle

Terminal control of the trajectory and rotational motion of an active spacecraft during a rendezvous with a passive spacecraft

General analytical forms for the solution of the Sylvester and Lyapunov equations for continuous and discrete dynamic systems

Attitude control algorithms for a descent vehicle returning from the moon

Band formulas for calculating the numerator’s coefficients of the transfer function of a single-input system

Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators

Solvability conditions of problem of synthesizing proportional-integral control of a linear MIMO system

Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: Analytical synthesis

Modification of the exact pole placement method and its application for the control of spacecraft motion

History of spacecraft control systems

Synthesis of linear postcompensators for signal processing of nonlinear systems of a special form

Output control of a spacecraft motion spectrum

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