Control system of spacecraft solar array drive assembly actuator
This paper deals with the issues of developing a control system of a spacecraft solar array drive assembly actuator that meets strict requirements for operation at the set angular accelerations and rotation velocities, under the influence of payload and disturbance forces. The work consists of d...
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| Format: | Article |
| Language: | English |
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Omsk State Technical University, Federal State Autonoumos Educational Institution of Higher Education
2019-11-01
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| Series: | Омский научный вестник |
| Subjects: | |
| Online Access: | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2019/5%20(167)/72-76%20%D0%9F%D0%BE%D0%BB%D0%BE%D0%B6%D0%B5%D0%BD%D1%86%D0%B5%D0%B2%20%D0%94.%20%D0%A1.,%20%D0%94%D0%B6%D1%83%D0%BA%D0%B8%D1%87%20%D0%94.%20%D0%99.,%20%D0%97%D0%B0%D1%85%D0%B0%D1%80%D0%BE%D0%B2%20%D0%94.%20%D0%9D..pdf |
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| _version_ | 1832572857861799936 |
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| author | D. S. Polozhentsev D. J. Dzhukich D. N. Zakharov |
| author_facet | D. S. Polozhentsev D. J. Dzhukich D. N. Zakharov |
| author_sort | D. S. Polozhentsev |
| collection | DOAJ |
| description | This paper deals with the issues of developing a control system of
a spacecraft solar array drive assembly actuator that meets strict requirements for operation at the set angular accelerations and
rotation velocities, under the influence of payload and disturbance
forces. The work consists of developing a control system, its
mathematical description, simulation and fabrication of an assembly
prototype that meets the defined technical specifications. In the
work, methods of mathematical and experimental investigation
are applied. System mathematical simulation was carried out using
the Matlab/Simulink applied software. As a result of the work, a
structural diagram is proposed of the control system of a spacecraft
SADA actuator of an operating follow-up system based on the
set angular position that is calculated as required for operation
at the defined angular accelerations and rotation velocities. The
article presents the results of mathematical simulation of actuator
operation, the results obtained during operation at the defined
angular rotation velocity by a prototype SADA, the analysis and
comparison of theoretical and practical results. Experimental
investigation shows the achievement of the goal when developing
the actuator control system, as well as rather exact matching of
simulation and experiment results. The proposed control system
can be used when designing and developing devices with similar
technical specifications. |
| format | Article |
| id | doaj-art-1227cfe3db4c48beb4aa54a0a8b7aa2c |
| institution | Kabale University |
| issn | 1813-8225 2541-7541 |
| language | English |
| publishDate | 2019-11-01 |
| publisher | Omsk State Technical University, Federal State Autonoumos Educational Institution of Higher Education |
| record_format | Article |
| series | Омский научный вестник |
| spelling | doaj-art-1227cfe3db4c48beb4aa54a0a8b7aa2c2025-02-02T06:22:51ZengOmsk State Technical University, Federal State Autonoumos Educational Institution of Higher EducationОмский научный вестник1813-82252541-75412019-11-015 (167)727610.25206/1813-8225-2019-167-72-76Control system of spacecraft solar array drive assembly actuatorD. S. Polozhentsev0D. J. Dzhukich1D. N. Zakharov2JSC «Command Devices Research Institute»; Baltic State Technical University «VOENMEH» named after D. F. Ustinov; State University of Aerospace InstrumentationJSC «Command Devices Research Institute»; Baltic State Technical University «VOENMEH» named after D. F. UstinovBaltic State Technical University «VOENMEH» named after D. F. UstinovThis paper deals with the issues of developing a control system of a spacecraft solar array drive assembly actuator that meets strict requirements for operation at the set angular accelerations and rotation velocities, under the influence of payload and disturbance forces. The work consists of developing a control system, its mathematical description, simulation and fabrication of an assembly prototype that meets the defined technical specifications. In the work, methods of mathematical and experimental investigation are applied. System mathematical simulation was carried out using the Matlab/Simulink applied software. As a result of the work, a structural diagram is proposed of the control system of a spacecraft SADA actuator of an operating follow-up system based on the set angular position that is calculated as required for operation at the defined angular accelerations and rotation velocities. The article presents the results of mathematical simulation of actuator operation, the results obtained during operation at the defined angular rotation velocity by a prototype SADA, the analysis and comparison of theoretical and practical results. Experimental investigation shows the achievement of the goal when developing the actuator control system, as well as rather exact matching of simulation and experiment results. The proposed control system can be used when designing and developing devices with similar technical specifications.https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2019/5%20(167)/72-76%20%D0%9F%D0%BE%D0%BB%D0%BE%D0%B6%D0%B5%D0%BD%D1%86%D0%B5%D0%B2%20%D0%94.%20%D0%A1.,%20%D0%94%D0%B6%D1%83%D0%BA%D0%B8%D1%87%20%D0%94.%20%D0%99.,%20%D0%97%D0%B0%D1%85%D0%B0%D1%80%D0%BE%D0%B2%20%D0%94.%20%D0%9D..pdfelectric drivesolar array drive assemblysadabrushless dc electric motorangular velocity control systemangular acceleration control systemangle feedback |
| spellingShingle | D. S. Polozhentsev D. J. Dzhukich D. N. Zakharov Control system of spacecraft solar array drive assembly actuator Омский научный вестник electric drive solar array drive assembly sada brushless dc electric motor angular velocity control system angular acceleration control system angle feedback |
| title | Control system of spacecraft solar array drive assembly actuator |
| title_full | Control system of spacecraft solar array drive assembly actuator |
| title_fullStr | Control system of spacecraft solar array drive assembly actuator |
| title_full_unstemmed | Control system of spacecraft solar array drive assembly actuator |
| title_short | Control system of spacecraft solar array drive assembly actuator |
| title_sort | control system of spacecraft solar array drive assembly actuator |
| topic | electric drive solar array drive assembly sada brushless dc electric motor angular velocity control system angular acceleration control system angle feedback |
| url | https://www.omgtu.ru/general_information/media_omgtu/journal_of_omsk_research_journal/files/arhiv/2019/5%20(167)/72-76%20%D0%9F%D0%BE%D0%BB%D0%BE%D0%B6%D0%B5%D0%BD%D1%86%D0%B5%D0%B2%20%D0%94.%20%D0%A1.,%20%D0%94%D0%B6%D1%83%D0%BA%D0%B8%D1%87%20%D0%94.%20%D0%99.,%20%D0%97%D0%B0%D1%85%D0%B0%D1%80%D0%BE%D0%B2%20%D0%94.%20%D0%9D..pdf |
| work_keys_str_mv | AT dspolozhentsev controlsystemofspacecraftsolararraydriveassemblyactuator AT djdzhukich controlsystemofspacecraftsolararraydriveassemblyactuator AT dnzakharov controlsystemofspacecraftsolararraydriveassemblyactuator |