Method for Validation of the Onboard Attitude Control System Software of the Auriga Earth Remote Sensing Small Spacecraft

2017 ◽  
Vol 51 (7) ◽  
pp. 646-653
Author(s):  
P. E. Rozin
Keyword(s):  
Remote Sensing ◽  
Control System ◽  
Attitude Control ◽  
System Software ◽  
Attitude Control System ◽  
Earth Remote Sensing ◽  
Small Spacecraft

An approach to forming the design performance of the attitude control system for small spacecraft

2015 ◽  
Vol 58 (4) ◽  
pp. 376-382 ◽  
Author(s):  
O. M. Alifanov ◽  
Yu. G. Egorov ◽  
V. M. Kul’kov ◽  
V. V. Terent’ev ◽  
S. O. Firsyuk
Keyword(s):  
Control System ◽  
Attitude Control ◽  
Attitude Control System ◽  
Design Performance ◽  
Small Spacecraft

scholarly journals Modelling the attitude dynamics of small spacecraft with a magnetic attitude control system in three-axis stabilization mode

2019 ◽  
Vol 488 (4) ◽  
pp. 377-382
Author(s):  
V. M. Kulkov ◽  
Yu. G. Egorov ◽  
S. O. Firsyuk ◽  
V. V. Terentyev ◽  
A. O. Shemyakov
Keyword(s):  
Magnetic Field ◽  
Mathematical Model ◽  
Control System ◽  
Attitude Control ◽  
Control Law ◽  
Attitude Dynamics ◽  
Attitude Control System ◽  
Small Spacecraft ◽  
Magnetic Attitude Control ◽  
System Movement

The problem of modeling the attitude-control modes of small spacecraft with the use of electromagnetic systems, interacting with the Earths magnetic field is considered. A small spacecraft angular motion mathematical model is developed. A control law for magnetic attitude control system of small spacecraft is formulated. Results of satellite with magnetic attitude control system movement numerical modelling are presented.

scholarly journals Modeling the angular momentum control of small spacecraft with a magnetic attitude control system

2019 ◽  
Vol 484 (4) ◽  
pp. 415-419
Author(s):  
V. M. Kulkov ◽  
Yu. G. Egorov ◽  
S. O. Firsyuk ◽  
V. V. Terentyev ◽  
A. O. Shemyakov
Keyword(s):  
Angular Momentum ◽  
Control System ◽  
Attitude Control ◽  
Experimental Studies ◽  
Control Mode ◽  
System Control ◽  
Attitude Control System ◽  
Electromagnetic System ◽  
Small Spacecraft ◽  
Magnetic Attitude Control

The problem of modeling the angular momentum control modes of small spacecraft using electromagnetic systems interacting with the Earth’s magnetic field is considered. The electromagnetic system control law has been constructed for various compositions of measurable parameters. A set of scale factors has been formed to investigate the angular momentum control mode of dynamically similar models. Based on a dynamical test stand, we have carried out experimental studies to model the angular motion dynamics of small spacecraft with a magnetic attitude control system.

Modeling the Angular Momentum Control of Small Spacecraft with a Magnetic Attitude Control System

2019 ◽  
Vol 64 (2) ◽  
pp. 57-60
Author(s):  
V. M. Kulkov ◽  
Yu. G. Egorov ◽  
S. O. Firsyuk ◽  
V. V. Terentyev ◽  
A. O. Shemyakov
Keyword(s):  
Angular Momentum ◽  
Control System ◽  
Attitude Control ◽  
Attitude Control System ◽  
Small Spacecraft ◽  
Magnetic Attitude Control

Investigation of the structural and functional reliability of small spacecraft in solving orientation problems

2020 ◽  
Vol 5 ◽  
pp. 132-140
Author(s):  
A.N. Pavlov ◽  
◽  
A.Yu. Kylakov ◽  
V.N. Vorotyagin ◽  
A.B. Umarov ◽  
...  
Keyword(s):  
Control System ◽  
Attitude Control ◽  
Attitude Control System ◽  
Modes Of Operation ◽  
Small Spacecraft ◽  
Functional Reliability

At the stages of design, creation and application of small spacecraft to develop solutions aimed at increasing their stability, it is necessary to assess the indicators of structural and functional reliability of elements of onboard systems, taking into account the involvement of various modes of operation. This article presents the results of a study of the influence of confi gurations of sensors of the attitude control system on the structural and functional reliability of a small spacecraft when solving task of determining the attitude in various modes of operation.

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