| Issue |
Title |
File |
| Vol 58, No 6 (2019) |
Analytical Algorithm for Constructing the Orbital Orientation of a Spacecraft with an Incomplete Measurement of the State Vector Components |
(Eng)
|
|
Zubov N.E., Lapin A.V., Ryabchenko V.N.
|
| Vol 58, No 6 (2019) |
Synthesis of the Optimal Control of the Spacecraft Orientation Using Combined Criteria of Quality |
(Eng)
|
|
Levskii M.V.
|
| Vol 58, No 6 (2019) |
Implementation of the Orbital Orientation Mode of an Artificial Satellite of the Earth without Accumulation of the Angular Momentum of the Gyro System |
(Eng)
|
|
Ignatov A.I., Sazonov V.V.
|
| Vol 58, No 5 (2019) |
Passive System for the Angular Damping of the SAMSAT-QB50 Nanosattelite |
(Eng)
|
|
Belokonov I.V., Ivanov D.S., Ovchinnikov M.Y., Pen’kov V.I.
|
| Vol 58, No 5 (2019) |
Application of The Method of Optimized Delta-Transformations in the Control Landing Problem for an Unmanned Aerial Vehicle |
(Eng)
|
|
Kravchenko P.P., Kulikov L.I., Scherbinin V.V.
|
| Vol 58, No 5 (2019) |
Algorithm for Controlling a Spacecraft’s Engine with Preventing the Angular Momentum Accumulation |
(Eng)
|
|
Ulybyshev S.Y.
|
| Vol 58, No 4 (2019) |
Universal Algorithm for Failure Detection in Duplicated Sensors of a Tracking System |
(Eng)
|
|
Volobuev M.F.
|
| Vol 58, No 3 (2019) |
Low-Altitude Aircraft Routing |
(Eng)
|
|
Petrov M.Y.
|
| Vol 58, No 3 (2019) |
Algorithms of Stabilization of a Spacecraft with Flexible Elements |
(Eng)
|
|
Ovchinnikov M.Y., Tkachev S.S., Shestopyorov A.I.
|
| Vol 58, No 3 (2019) |
Calculation of Program Controls Not Generating Singular States of a Gyro System. II |
(Eng)
|
|
Belyaev B.B., Bychkov I.V., Druzhinin E.I., Ul’yanov S.A.
|
| Vol 58, No 2 (2019) |
Reorientation of a Rigid Body Controlled by a Movable Internal Mass |
(Eng)
|
|
Naumov N.Y., Chernous’ko F.L.
|
| Vol 58, No 2 (2019) |
Calculation of Program Control Not Generating Singularities in Gyrosystems |
(Eng)
|
|
Druzhinin E.I.
|
| Vol 58, No 2 (2019) |
Stabilizing the Motion of a Low-Orbit Electrodynamic Tether System |
(Eng)
|
|
Voevodin P.S., Zabolotnov Y.M.
|
| Vol 58, No 2 (2019) |
Reconstruction of a Spacecraft’s Attitude Motion Using the Data on the Current Collected from Solar Panels |
(Eng)
|
|
Belokonov I.V., Kramlikh A.V., Lomaka I.A., Nikolaev P.N.
|
| Vol 58, No 1 (2019) |
Restricted Quadratic Optimal Control of a Spacecraft Turning in a Fixed Time Period |
(Eng)
|
|
Levskii M.V.
|
| Vol 58, No 1 (2019) |
Online Two-Dimensional Route Planning for a Group of Unmanned Aerial Vehicles |
(Eng)
|
|
Goncharenko V.I., Lebedev G.N., Mikhailin D.A.
|
| Vol 57, No 6 (2018) |
A Solution to the Problem of Assessing Aviation Safety by Simulation Modeling |
(Eng)
|
|
Vishnyakova L.V., Obukhov Y.V.
|
| Vol 57, No 6 (2018) |
Mission Design of Multipurpose Flights to Venus |
(Eng)
|
|
Golubev Y.F., Grushevskii A.V., Koryanov V.V., Tuchin A.G., Tuchin D.A.
|
| Vol 57, No 6 (2018) |
Two Direct Low Thrust Trajectory Optimization Techniques |
(Eng)
|
|
Trofimov S.P., Tselousova A.A., Shirobokov M.G.
|
| Vol 57, No 5 (2018) |
Guaranteeing UAV Trajectory Control When Approaching a Maneuvering Air Target |
(Eng)
|
|
Evdokimenkov V.N., Krasilshchikov M.N., Lyapin N.A.
|
| Vol 57, No 5 (2018) |
Indicatory Horizontal Stabilization of the Platform with Two Degrees of Freedom of a Uniaxial Wheel Module at Its Displacements on a Nonhorizontal, Uneven Surface |
(Eng)
|
|
Aleshin B.S., Mikheev V.V., Chernomorskii A.I.
|
| Vol 57, No 3 (2018) |
Long-Term Linear-Quadratic Control of Satellite Constellations in Highly Elliptical Orbits |
(Eng)
|
|
Gunchenko M.Y., Ulybyshev Y.P.
|
| Vol 57, No 2 (2018) |
Active-Passive System of Safe Nap-of-the-Earth Piloting |
(Eng)
|
|
Kim V.Y., Lisitsyn V.M., Muzhichek S.M., Obrosov K.V.
|
| Vol 57, No 2 (2018) |
Estimating the Domain of Admissible Parameters of a Control System of a Vibratory Robot |
(Eng)
|
|
Golitsyna M.V., Samsonov V.A.
|
| Vol 57, No 2 (2018) |
The Onboard Algorithm for Averaging the Orbital Motion Parameters of the International Space Station in the ICARUS Experiment |
(Eng)
|
|
Sumarokov A.V.
|
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