Modeling of a Solar Arrays Deployment Process at Ground Tests of Mechanical Devices on Active Gravity Compensation Systems; Russian-Pacific Conference on Computer Technology and Applications, RPC 2018
| Parent link: | Russian-Pacific Conference on Computer Technology and Applications, RPC 2018.— 2018.— [4 p.] |
|---|---|
| Egile korporatiboa: | , |
| Beste egile batzuk: | , , , |
| Gaia: | Title screen This paper focuses on the modeling of a spacecraft solar arrays deployment process in ground tests of mechanical devices on the active gravity compensation systems. The ground tests are carried out on the test workbenches. Such workbenches provide a gravity compensation of the solar arrays in the deployment process in order to simulate the space weightlessness conditions. The passive gravity compensation systems with cable suspensions for moving parts of the solar array are the most widespread at nowadays. The gravity compensation of the passive workbenches for the large size and heavy solar arrays could differ significantly from the space weightlessness conditions because of the “added mass effect”. For this reason, an active gravity compensation workbench was created by the ISS-Reshetnev Company order [1]. In the active gravity compensation system, the trolleys are equipped with tracking systems, which hold the suspension cable on vertical position with high accuracy during the solar array deployment and the tensile (compensation) forces in the cables supported by automatic control systems at desired levels. The modeling of dynamics of the solar arrays transformable elements and the active gravity compensation system mobile devices was implemented in Matlab Simulink with creating mechanical component models at SolidWorks and other. Режим доступа: по договору с организацией-держателем ресурса |
| Hizkuntza: | ingelesa |
| Argitaratua: |
2018
|
| Gaiak: | |
| Sarrera elektronikoa: | https://doi.org/10.1109/RPC.2018.8482118 |
| Formatua: | MixedMaterials Baliabide elektronikoa Liburu kapitulua |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=659624 |
MARC
| LEADER | 00000naa0a2200000 4500 | ||
|---|---|---|---|
| 001 | 659624 | ||
| 005 | 20250827134251.0 | ||
| 035 | |a (RuTPU)RU\TPU\network\28291 | ||
| 035 | |a RU\TPU\network\9047 | ||
| 090 | |a 659624 | ||
| 100 | |a 20190312d2018 k||y0engy50 ba | ||
| 101 | 0 | |a eng | |
| 135 | |a drcn ---uucaa | ||
| 181 | 0 | |a i | |
| 182 | 0 | |a b | |
| 200 | 1 | |a Modeling of a Solar Arrays Deployment Process at Ground Tests of Mechanical Devices on Active Gravity Compensation Systems |f I. K. Shpyakin [et al.] | |
| 203 | |a Text |c electronic | ||
| 300 | |a Title screen | ||
| 320 | |a [References: 10 tit.] | ||
| 330 | |a This paper focuses on the modeling of a spacecraft solar arrays deployment process in ground tests of mechanical devices on the active gravity compensation systems. The ground tests are carried out on the test workbenches. Such workbenches provide a gravity compensation of the solar arrays in the deployment process in order to simulate the space weightlessness conditions. The passive gravity compensation systems with cable suspensions for moving parts of the solar array are the most widespread at nowadays. The gravity compensation of the passive workbenches for the large size and heavy solar arrays could differ significantly from the space weightlessness conditions because of the “added mass effect”. For this reason, an active gravity compensation workbench was created by the ISS-Reshetnev Company order [1]. In the active gravity compensation system, the trolleys are equipped with tracking systems, which hold the suspension cable on vertical position with high accuracy during the solar array deployment and the tensile (compensation) forces in the cables supported by automatic control systems at desired levels. The modeling of dynamics of the solar arrays transformable elements and the active gravity compensation system mobile devices was implemented in Matlab Simulink with creating mechanical component models at SolidWorks and other. | ||
| 333 | |a Режим доступа: по договору с организацией-держателем ресурса | ||
| 463 | |t Russian-Pacific Conference on Computer Technology and Applications, RPC 2018 |o Proceedings of the 3rd Conference, Vladivostok, Russia 18-25 August, 2018 |v [4 p.] |d 2018 | ||
| 610 | 1 | |a электронный ресурс | |
| 610 | 1 | |a труды учёных ТПУ | |
| 610 | 1 | |a zero-gravity | |
| 610 | 1 | |a weightlessness environment | |
| 610 | 1 | |a gravity compensation system | |
| 610 | 1 | |a deployable solar arrays | |
| 610 | 1 | |a ground test | |
| 610 | 1 | |a гравитация | |
| 610 | 1 | |a солнечные батареи | |
| 610 | 1 | |a испытания | |
| 701 | 1 | |a Shpyakin |b I. K. |g Ivan Konstantinovich | |
| 701 | 1 | |a Voronin |b A. V. |c Specialist in the field of informatics and computer technology |c Associate Professor of Tomsk Polytechnic University, Candidate of technical sciences |f 1947- |g Aleksandr Vasilyevich |3 (RuTPU)RU\TPU\pers\31642 |9 15780 | |
| 701 | 1 | |a Malishenko (Malyshenko) |b A. M. |c specialist in the field of informatics and computer technology |c Professor of Tomsk Polytechnic University, Doctor of technical sciences |c Corresponding member of the Academy of Electrical Engineering Sciences of the Russian Federation |c Full member of the International Higher Education Academy of Sciences |f 1937- |g Alexanedr Maximovich |3 (RuTPU)RU\TPU\pers\31592 |9 15751 | |
| 701 | 1 | |a Maykov |b S. A. |g Stepan Aleksandrovich | |
| 712 | 0 | 2 | |a Национальный исследовательский Томский политехнический университет (ТПУ) |b Институт кибернетики (ИК) |b Кафедра интегрированных компьютерных систем управления (ИКСУ) |3 (RuTPU)RU\TPU\col\18701 |
| 712 | 0 | 2 | |a Национальный исследовательский Томский политехнический университет |b Инженерная школа информационных технологий и робототехники |b Отделение автоматизации и робототехники (ОАР) |3 (RuTPU)RU\TPU\col\23553 |
| 801 | 2 | |a RU |b 63413507 |c 20190312 |g RCR | |
| 856 | 4 | |u https://doi.org/10.1109/RPC.2018.8482118 | |
| 942 | |c CF | ||