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- Article name
- RESULTS OF LAND TESTS OF THE HIGH-PRECISION STAR SENSOR
- Authors
- Razzhivalov P. N., , razzhivalovpavel@gmail.com, National Research University of Electronic Technology; Scientific and Production Enterprise "Optical-Electronic Complexes and Systems", Moscow, Russia
Knjazev A. N., , knyazev@minprom.gov.ru, The Ministry of Industry and Trade of the Russian Federation, Moscow, Russia
Baklanov A. I., , optecs@mail.ru, Joint Stock Company Space Rocket Centre Progress - Scientific and Production Enterprise "OPTEKS", Moscow, Russia
Verhovtseva A. V., , alevteena@gmail.com, Joint Stock Company Space Rocket Centre Progress - Scientific and Production Enterprise "OPTEKS", Moscow, Russia
Zabiyakin A. S., , , Joint Stock Company Space Rocket Centre Progress - Scientific and Production Enterprise "OPTEKS", Moscow, Russia
Tsiliurik A. I., , tsiliur@gmail.com, Joint Stock Company Space Rocket Centre Progress - Scientific and Production Enterprise "OPTEKS", Moscow, Russia
- Keywords
- star device / star sensor / orientation device / calibration / the test stand / land optimization
- Year
- 2016 Issue 2 Pages 72 - 78
- Code EDN
- Code DOI
- Abstract
- It is difficult to present modern systems of orientation and navigation of the spacecrafts without the star sensors of various accuracy providing three-axis orientation of spacecrafts. In spacecrafts of the remote sensing of Earth, modern star sensors play an important role at the solution of problems of keeping of the set spatial orientation of the equipment installed on the spacecraft and a coordinate binding of the pictures received by this equipment. The requirements for the accuracy of a coordinate binding are higher, the above there has to be an accuracy of the star sensor. In 2010-2014 in Scientific and Production Enterprise "OPTEKS" the star sensor of high precision for perspective spacecrafts of high spatial resolution was developed and manufactured. In the real work by authors last results of ground tests are presented, namely: results of work of cooling for the star sensor and results of precision measurements on single object executed on installation of measurement of angular coordinates.
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