Mathematical modeling of a controlled electromechanical actuator for special assembly and coupling equipment
- Authors: Nosov A.S.1
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Affiliations:
- Branch of the Ground-based Space Infrastructure Operation Center – Design Bureau “KB “Motor”
- Issue: Vol 16, No 2 (2017)
- Pages: 81-89
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/5122
- DOI: https://doi.org/10.18287/2541-7533-2017-16-2-81-89
- ID: 5122
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Abstract
The article presents theoretical and experimental bases for the creation of a driving gear with an actuating mechanism based on a planetary roller drive to improve the fidelity of the specified motion law and velocity performance of the support equipment actuators and engineering systems of missile and space-rocket complexes, as well as for integrated tests of heavy missiles. We present a mathematical model of a controlled electromechanical actuator for special assembly and coupling equipment. The results of the tests carried out lead to the conclusion that in order to create a high precision electromechanical drive, it is necessary to use transmission with a smaller gap between the mating elements, high accuracy and reliability of operation. A new design of a planetary roller drive and the advantages of using a stepper motor are described. Thus, mathematical modeling of an electromechanical actuator with a planetary roller drive with a mockup test on an assembly and coupling tilting device makes it possible to create an electromechanical actuator with improved technical and operational characteristics for a tilting device of the space head of a super heavy launch vehicle. This reduces the probability of emergency situations during conducting government and commercial space programs.
About the authors
A. S. Nosov
Branch of the Ground-based Space Infrastructure Operation Center – Design Bureau “KB “Motor”
Author for correspondence.
Email: alekstambov@mail.ru
Supervisor of the innovative technologies section
Russian FederationReferences
- Biryukov G.P., Manaenkov E.N., Fadeev A.S. Tekhnologicheskoe oborudovanie otechestvennykh raketno-kosmicheskikh kompleksov: uch. posobie dlya vuzov [Support equipment of domestic space-rocket complexes]. Moscow: Restart Publ., 2012. 599 p.
- Nosov A.S. Justification techniques for the structure, configuration and parameters of a drivegear with roller drive of increased accuracy and operational reliability selection. Vestnik Moskovskogo Aviatsionnogo Instituta. 2016. V. 23, no. 1. P. 170-176. (In Russ.)
- Nosov A.S. Power electromechanical drive based on planetary roller-screw gear of improved accuracy. Vestnik Moskovskogo Aviatsionnogo Instituta. 2015. V. 22, no. 4. P. 100-107. (In Russ.)
- Kozyrev V.V. Konstruktsii rolikovintovykh peredach i metodika ikh proektirovaniya: uch. posobie [Roller drive designs and the design technique]. Vladimir: Vladimir State University Publ., 2004. 101 p.
- Petrenko A.M. Spetsial'ny evintovye mekhanizmy v silovykh privodakh: uch. posobie [Special screw mechanisms in actuators]. Moscow: Moscow Automobile and Road Institute Publ., 1997. 86 p.