Design and analysis of power supply and information transfer to three-axis gyroscope stabilizer platform; MATEC Web of Conferences; Vol. 48 : Space Engineering
| Parent link: | MATEC Web of Conferences Vol. 48 : Space Engineering.— 2016.— [01001, 10 p.] |
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| Corporate Author: | |
| Other Authors: | , , , |
| Summary: | Title screen The paper focuses on problems of the engineering implementation of 3-axis gyrostabilizer of the camera for orthophotography performed from light and ultralight aircrafts. The functional diagram of gyrostabilizer is characterized by a lighter ball-bearing having a large inner diameter used for the platform suspension on its internal (vertical) axis. The problem is to transfer the supply voltage to the platform and the electric signals to and from the platform. Design solutions concerning the power supply and information transfer are supported by the experimental techniques suggested in this paper, namely: the use of the rolling contact; three-phase gyro motor power supply replaced by that from the single-phase network; signal transmission from the precession angle sensor using the air transformer; current and voltage frequency division; DC mode selection for the torquer. The results obtained prove the efficiency of the suggested design solutions. |
| Language: | English |
| Published: |
2016
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| Series: | Spacecrafts and Devices |
| Subjects: | |
| Online Access: | http://dx.doi.org/10.1051/matecconf/20164801001 http://earchive.tpu.ru/handle/11683/33689 |
| Format: | MixedMaterials Electronic Book Chapter |
| KOHA link: | https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=648891 |
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| 200 | 1 | |a Design and analysis of power supply and information transfer to three-axis gyroscope stabilizer platform |f L. N. Belyanin [et al.] | |
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| 225 | 1 | |a Spacecrafts and Devices | |
| 300 | |a Title screen | ||
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| 330 | |a The paper focuses on problems of the engineering implementation of 3-axis gyrostabilizer of the camera for orthophotography performed from light and ultralight aircrafts. The functional diagram of gyrostabilizer is characterized by a lighter ball-bearing having a large inner diameter used for the platform suspension on its internal (vertical) axis. The problem is to transfer the supply voltage to the platform and the electric signals to and from the platform. Design solutions concerning the power supply and information transfer are supported by the experimental techniques suggested in this paper, namely: the use of the rolling contact; three-phase gyro motor power supply replaced by that from the single-phase network; signal transmission from the precession angle sensor using the air transformer; current and voltage frequency division; DC mode selection for the torquer. The results obtained prove the efficiency of the suggested design solutions. | ||
| 461 | 0 | |0 (RuTPU)RU\TPU\network\4526 |t MATEC Web of Conferences | |
| 463 | 0 | |0 (RuTPU)RU\TPU\network\13956 |t Vol. 48 : Space Engineering |o IV Russian Forum for Young Scientists with International Participation, April 12-14, 2016, Tomsk, Russia |o [proceedings] |f National Research Tomsk Polytechnic University (TPU) ; eds. V. N. Borikov [et al.] |v [01001, 10 p.] |d 2016 | |
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| 610 | 1 | |a гироскопы | |
| 610 | 1 | |a стабилизаторы | |
| 610 | 1 | |a платформы | |
| 610 | 1 | |a летательные аппараты | |
| 610 | 1 | |a двигатели | |
| 610 | 1 | |a электрические сигналы | |
| 701 | 1 | |a Belyanin |b L. N. |c specialist in the field of instrument making |c Associate Professor of Tomsk Polytechnic University, Candidate of technical sciences |f 1944- |g Lev Nikolaevich |3 (RuTPU)RU\TPU\pers\35231 | |
| 701 | 0 | |a Ket Vu Doan | |
| 701 | 1 | |a Pozharskiy |b T. |g Timofey | |
| 701 | 0 | |a Trong Yen Nguyen | |
| 712 | 0 | 2 | |a Национальный исследовательский Томский политехнический университет |c (2009- ) |9 26305 |
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| 856 | 4 | |u http://dx.doi.org/10.1051/matecconf/20164801001 | |
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