Issue |
Title |
File |
Vol 57, No 2 (2018) |
Analytic Controlling Reorientation of a Spacecraft Using a Combined Criterion of Optimality |
![PDF](/img/labels/pdf.png) (Eng)
|
Levskii M.V.
|
Vol 57, No 1 (2018) |
Quadratic Optimal Control in Reorienting a Spacecraft in a Fixed Time Period in a Dynamic Problem Statement |
![PDF](/img/labels/pdf.png) (Eng)
|
Levskii M.V.
|
Vol 57, No 1 (2018) |
Laboratory Facility for Microsatellite Mock-up Motion Simulation |
![PDF](/img/labels/pdf.png) (Eng)
|
Ivanov D.S., Koptev M.D., Mashtakov Y.V., Ovchinnikov M.Y., Proshunin N.N., Tkachev S.S., Fedoseev A.I., Shachkov M.O.
|
Vol 56, No 6 (2017) |
Two-dimensional path finding subject to geometric constraints |
![PDF](/img/labels/pdf.png) (Eng)
|
Andreychuk A.A., Yakovlev K.S.
|
Vol 56, No 5 (2017) |
Aerial object ranging based on goniometric data in an airborne single-position passive optoelectronic system |
![PDF](/img/labels/pdf.png) (Eng)
|
Lisitsyn V.M., Vinetskii Y.R.
|
Vol 56, No 5 (2017) |
Control and trajectory optimization of an aircraft’s alignment with the desired track |
![PDF](/img/labels/pdf.png) (Eng)
|
Volodina Y.O., Golubeva A.A., Kulanov N.V.
|
Vol 56, No 5 (2017) |
A predictive algorithm for runway overrun protection |
![PDF](/img/labels/pdf.png) (Eng)
|
Bukov V.N., Bykov V.N.
|
Vol 56, No 5 (2017) |
Adaptive three-dimensional guidance of flying vehicle at fixed point with specified approach direction |
![PDF](/img/labels/pdf.png) (Eng)
|
Ulybyshev Y.P.
|
Vol 56, No 5 (2017) |
On the rapid orbital attitude control of manned and cargo spacecraft Soyuz MS and Progress MS |
![PDF](/img/labels/pdf.png) (Eng)
|
Borisenko N.Y., Sumarokov A.V.
|
Vol 56, No 4 (2017) |
Terminal synthesis of orbital orientation for a spacecraft |
![PDF](/img/labels/pdf.png) (Eng)
|
Zubov N.E., Li M.V., Mikrin E.A., Ryabchenko V.N.
|
Vol 56, No 3 (2017) |
A method to maneuver aeroballistic missiles under counteractions |
![PDF](/img/labels/pdf.png) (Eng)
|
Goncharenko V.I., Gorchenko L.D.
|
Vol 56, No 3 (2017) |
Methods for suppressing nonlinear oscillations in astatic auto-piloted aircraft control systems |
![PDF](/img/labels/pdf.png) (Eng)
|
Andrievsky B.R., Kuznetsov N.V., Leonov G.A.
|
Vol 56, No 3 (2017) |
Horizontal stabilization of the two-degree-of-freedom platform of a uniaxial wheeled module tracking a given trajectory over an underlying surface |
![PDF](/img/labels/pdf.png) (Eng)
|
Aleshin B.S., Maksimov V.N., Mikheev V.V., Chernomorskii A.I.
|
Vol 56, No 3 (2017) |
Attitude control algorithms for a descent vehicle returning from the moon |
![PDF](/img/labels/pdf.png) (Eng)
|
Evdokimov S.N., Klimanov S.I., Korchagin A.N., Mikrin E.A., Sikharulidze Y.G., Tuchin A.G.
|
Vol 56, No 3 (2017) |
Synthesis of algorithms for the detection and resolution of collision conflicts based on data from the automatic dependent surveillance system under uncertainty |
![PDF](/img/labels/pdf.png) (Eng)
|
Burkin V.S.
|
Vol 56, No 2 (2017) |
Formation of high inclined orbits to the ecliptic by multiple gravity assist maneuvers |
![PDF](/img/labels/pdf.png) (Eng)
|
Golubev Y.F., Grushevskii A.V., Koryanov V.V., Tuchin A.G., Tuchin D.A.
|
Vol 56, No 2 (2017) |
Construction of the initial deorbit region for landing at the given place |
![PDF](/img/labels/pdf.png) (Eng)
|
Evdokimov S.N., Klimanov S.I., Korchagin A.N., Mikrin E.A., Sikharulidze Y.G., Tuchin A.G.
|
Vol 56, No 2 (2017) |
Methods for the vibration determination and parameter identification of spacecraft with flexible structures |
![PDF](/img/labels/pdf.png) (Eng)
|
Ivanov D.S., Meus S.V., Ovchinnikov A.V., Ovchinnikov M.Y., Shestakov S.A., Yakimov E.N.
|
Vol 56, No 1 (2017) |
Estimates of near-circular orbits after a single correction: a geometrical method |
![PDF](/img/labels/pdf.png) (Eng)
|
Baranov A.A., Vikhrachev V.O., Karatunov M.O., Razumnyi Y.N.
|
Vol 55, No 6 (2016) |
Analytical solution of the optimal slew problem for an axisymmetric spacecraft in the class of conical motions |
![PDF](/img/labels/pdf.png) (Eng)
|
Molodenkov A.V., Sapunkov Y.G.
|
Vol 55, No 5 (2016) |
Solvability conditions of problem of synthesizing proportional-integral control of a linear MIMO system |
![PDF](/img/labels/pdf.png) (Eng)
|
Zubov N.E., Mikrin E.A., Misrikhanov M.S., Ryabchenko V.N.
|
Vol 55, No 5 (2016) |
Test complex for the onboard navigation system of an airport ground vehicle |
![PDF](/img/labels/pdf.png) (Eng)
|
Antonov D.A., Veremeenko K.K., Zharkov M.V., Zimin R.Y., Kuznetsov I.M., Pron’kin A.N.
|
Vol 55, No 4 (2016) |
Continuous monitoring of the state of aircraft and aviation groups |
![PDF](/img/labels/pdf.png) (Eng)
|
Buryak Y.I., Skrynnikov A.A.
|
Vol 55, No 3 (2016) |
Terminal control of the trajectory and rotational motion of an active spacecraft during a rendezvous with a passive spacecraft |
![PDF](/img/labels/pdf.png) (Eng)
|
Zubov N.E., Mikrin E.A., Oleinik A.S., Ryabchenko V.N.
|
Vol 55, No 3 (2016) |
An algorithm for estimating systematic measurement errors for air velocity, angle of attack, and sliding angle in flight testing |
![PDF](/img/labels/pdf.png) (Eng)
|
Korsun O.N., Nikolaev S.V., Pushkov S.G.
|
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