ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLY

The paper considers selection of parameters of the spacecraft periphery-type docking assembly. The kinematic scheme of its docking mechanism is based on the Gough-Stewart platform. Constructive implementation of its linear elements in operation is called the rods, and the controlled element is calle...

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Published in:Научно-технический вестник информационных технологий, механики и оптики
Main Authors: Yaroslav V. Rasskazov, Ivan E. Chernyshev
Format: Article
Language:English
Published: ITMO University 2020-02-01
Subjects:
Online Access:https://ntv.ifmo.ru/file/article/19350.pdf
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author Yaroslav V. Rasskazov
Ivan E. Chernyshev
author_facet Yaroslav V. Rasskazov
Ivan E. Chernyshev
author_sort Yaroslav V. Rasskazov
collection DOAJ
container_title Научно-технический вестник информационных технологий, механики и оптики
description The paper considers selection of parameters of the spacecraft periphery-type docking assembly. The kinematic scheme of its docking mechanism is based on the Gough-Stewart platform. Constructive implementation of its linear elements in operation is called the rods, and the controlled element is called a docking ring. The docking mechanism is characterized by the ability to accumulate the kinetic energy of spacecraft approach rather than to dampen it. To achieve this, an energy storage device is placed into each rod and incorporates a non-linear spiral spring mechanism. The energy storage device absorbs the kinetic energy of spacecraft approach and prevents its return after latching. The spiral spring mechanism implements a predetermined rod compression diagram and provides the necessary docking resistance force for spacecraft approach. The paper presents a general view of the rod compression diagram and the restrictions imposed on it. The model of the rod compression diagram is given, which is characterized by the introduction of a variable spring rate coefficient, and the method for identification of parameters is described. The method uses the calculation of the minimum mass of the spring mechanism. The method of parameters selection for a nonlinear spiral spring mechanism is given with predetermined dimension restrictions. The proposed methods can be used in the energy storage device optimization of the periphery-type docking assembly.
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spelling doaj-e88055ea228d41fabc2aa94c62b0502d2025-11-03T01:00:44ZengITMO UniversityНаучно-технический вестник информационных технологий, механики и оптики2226-14942500-03732020-02-0120113214010.17586/2226-1494-2020-20-1-132-140ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLYYaroslav V. Rasskazov0https://orcid.org/0000-0003-4774-4640Ivan E. Chernyshev1https://orcid.org/0000-0001-8289-1991Postgraduate, Head of Section — Deputy Department Head, S.P. Korolev Rocket and Space Public Corporation Energia, Korolev, 141070, Russian FederationLead Software Engineer, S.P. Korolev Rocket and Space Public Corporation Energia, Korolev, 141070, Russian FederationThe paper considers selection of parameters of the spacecraft periphery-type docking assembly. The kinematic scheme of its docking mechanism is based on the Gough-Stewart platform. Constructive implementation of its linear elements in operation is called the rods, and the controlled element is called a docking ring. The docking mechanism is characterized by the ability to accumulate the kinetic energy of spacecraft approach rather than to dampen it. To achieve this, an energy storage device is placed into each rod and incorporates a non-linear spiral spring mechanism. The energy storage device absorbs the kinetic energy of spacecraft approach and prevents its return after latching. The spiral spring mechanism implements a predetermined rod compression diagram and provides the necessary docking resistance force for spacecraft approach. The paper presents a general view of the rod compression diagram and the restrictions imposed on it. The model of the rod compression diagram is given, which is characterized by the introduction of a variable spring rate coefficient, and the method for identification of parameters is described. The method uses the calculation of the minimum mass of the spring mechanism. The method of parameters selection for a nonlinear spiral spring mechanism is given with predetermined dimension restrictions. The proposed methods can be used in the energy storage device optimization of the periphery-type docking assembly.https://ntv.ifmo.ru/file/article/19350.pdfspacecraftdocking mechanismparallel manipulatorgough-stewart platformparameters optimizationenergy accumulation
spellingShingle Yaroslav V. Rasskazov
Ivan E. Chernyshev
ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLY
spacecraft
docking mechanism
parallel manipulator
gough-stewart platform
parameters optimization
energy accumulation
title ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLY
title_full ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLY
title_fullStr ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLY
title_full_unstemmed ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLY
title_short ENERGY STORAGE DEVICE OPTIMIZATION IN PERIPHERY-TYPE DOCKING ASSEMBLY
title_sort energy storage device optimization in periphery type docking assembly
topic spacecraft
docking mechanism
parallel manipulator
gough-stewart platform
parameters optimization
energy accumulation
url https://ntv.ifmo.ru/file/article/19350.pdf
work_keys_str_mv AT yaroslavvrasskazov energystoragedeviceoptimizationinperipherytypedockingassembly
AT ivanechernyshev energystoragedeviceoptimizationinperipherytypedockingassembly