Mathematical model of the mirror system of the Millimetron observatory and a description of the method of pre-measurement of the telescope within this model
- 作者: Makarov S.N.1, Verhoglyad A.G.1, Stupak M.F.1, Ovchinnikov D.A.2, Oberemok Y.A.2
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隶属关系:
- Technological Design Institute of Scientific Instrument Engineering SB RAS
- JSC Academician M. F. Reshetnev “Information Satellite Systems”
- 期: 卷 22, 编号 1 (2021)
- 页面: 151-164
- 栏目: Section 2. Aviation and Space Technology
- ##submission.datePublished##: 15.03.2021
- URL: https://journals.eco-vector.com/2712-8970/article/view/562833
- DOI: https://doi.org/10.31772/2712-8970-2021-22-1-151-165
- ID: 562833
如何引用文章
详细
A mirror geometry control system for the Millimetron Observatory is being created to work as part of the on-board complex of scientific equipment. The system is designed to monitor the quality of the space telescope’s mirror system and use the data received as feedback signals for pre-setting and tuning the telescope’s optical system in outer space. The goal of the system is estimation of the multidimensional vector of unknown parameters of the telescope’s mirror system by indirect measurements obtained as a result of the measurement of the telescope by 3D scanning. A mathematical model has been created, numerically describing the process of pre-measurement of the mirror system of the Millimetron Observatory using optical control marks on the surface of the mirror system. The linear mathematical model allows to link the actual indirect measurements of the mirror system with the unknown biases of its parameters, determining the shape of the telescope. A formula has been developed for the optimal reverse problem solver in the process of pre-measurement of the mirror system. The method of measuring the components of the telescope as part of its pre-setting is described. The measurement of control marks is based on a onboard 3D scanner embedded in the design of the mirror system control system. The error analysis was carried out using the optimal solver, and a covariance matrix was obtained for the error vector of estimated parameter.
作者简介
Sergey Makarov
Technological Design Institute of Scientific Instrument Engineering SB RAS
Email: makarovsn@tdisie.nsc.ru
Senior Researcher
俄罗斯联邦, 41, Russian St., Novosibirsk, 630058Alexander Verhoglyad
Technological Design Institute of Scientific Instrument Engineering SB RAS
Email: verhog@tdisie.nsc.ru
Acting Deputy Director
俄罗斯联邦, 41, Russian St., Novosibirsk, 630058Mikhail Stupak
Technological Design Institute of Scientific Instrument Engineering SB RAS
编辑信件的主要联系方式.
Email: stupak@tdisie.nsc.ru
Cand. Sc., Associate Professor, Leading research Associate
俄罗斯联邦, 41, Russian St., Novosibirsk, 630058Dmitry Ovchinnikov
JSC Academician M. F. Reshetnev “Information Satellite Systems”
Email: dao@iss-reshetnev.ru
Deputy Head of Department 355
俄罗斯联邦, 52, Lenin St., Zheleznogorsk, Krasnoyarsk region, 662972Yuri Oberemok
JSC Academician M. F. Reshetnev “Information Satellite Systems”
Email: oberemok@iss-reshetnev.ru
Head of the Department
俄罗斯联邦, 52, Lenin St., Zheleznogorsk, Krasnoyarsk region, 662972参考
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