You are here

Spacecraft Dynamics and Control

Particularities of control of the International space station «Alpha» at the initial stage of flightI

¹Zlatkin Yu.M, ¹Rzhemovskiy VP, ¹Kuznetsov Yu.A. Particularities of control of the International space station «Alpha» at the initial stage of flightI. Kosm. nauka tehnol. 2006 ;12(2-3):003-007.

Mathematical model for estimation of the effect of aerodynamic aircraft control surfaces compensation on the level of their vibrations in case of transonic flutter

¹Safronov AV, ²Semon BY, ¹Nedilko AN. Mathematical model for estimation of the effect of aerodynamic aircraft control surfaces compensation on the level of their vibrations in case of transonic flutter. Space Science and Technology. 2018 ;24(4):14-23.

Synthesis of control of the angular motion of a spacecraft on the basis of generalization of the direct Lyapunov method

¹Volosov VV, ¹Shevchenko VM. Synthesis of control of the angular motion of a spacecraft on the basis of generalization of the direct Lyapunov method. Space Science and Technology. 2018 ;24(4):03-13.

Project-ballistic parameters of solving two space transport problems with the help of universal transport-power platforms

¹Dron NM, ¹Knysh LI, ¹Kondratyev AI, ²Zhuravel Ye.P, ³Moskalev SI, ²Tolmachov VV. Project-ballistic parameters of solving two space transport problems with the help of universal transport-power platforms. Kosm. nauka tehnol. 2004 ;10(4):060-065.

Some aspects of the influence of inpouring acoustic radiation on devices and systems of inertial navigation

¹Karachun VV, ¹Mel'nik VN, ¹Saverchenko VG. Some aspects of the influence of inpouring acoustic radiation on devices and systems of inertial navigation. Kosm. nauka tehnol. 2004 ;10(4):050-059.

High-altitude spacecraft power losses of solar arrays as a result of interaction with environment

¹Shuvalov VA, ²Kochubey GS, ²Priymak AI, ²Pismenniy NI. High-altitude spacecraft power losses of solar arrays as a result of interaction with environment. Kosm. nauka tehnol. 2004 ;10(4):039-049.

The control of essentially non-symmetric runaway block with the engine working uninterruptedly

¹Zlatkin Yu.M, ²Kalnoguz AN, ²Bataev VA, ²Kuzmin AI, ²Riumin MN, ²Yevtefeiev MP. The control of essentially non-symmetric runaway block with the engine working uninterruptedly. Kosm. nauka tehnol. 2004 ;10(4):032-038.

The algorithm for the determination of spacecraft orbit parameters with the use of the Doppler gauge system

¹Kovbasiuk SV, ²Makhonin EI, ¹Pysarchuk ОО. The algorithm for the determination of spacecraft orbit parameters with the use of the Doppler gauge system. Kosm. nauka tehnol. 2004 ;10(4):027-031.

Oscillations caused by flexible attached elements of satellite constructions

¹Shatikhin VE, ²Semenov LP, ³Artemenko YH, ⁴Borysenko VM, ³Helenko ОО. Oscillations caused by flexible attached elements of satellite constructions. Kosm. nauka tehnol. 2004 ;10(1):061-069.

Dynamics of a deformed space system of bodies with programmed change of the configuration

¹Dranovsky VI, ²Zakrzhevskii AE, ³Khoroshylov VS. Dynamics of a deformed space system of bodies with programmed change of the configuration. Kosm. nauka tehnol. 2004 ;10(1):045-053.

Pages