Skip to main content
Top
Published in: Artificial Life and Robotics 1/2020

29-10-2019 | Original Article

A study of a gravity compensation system for the spacecraft prototype test by using multi-robot system

Authors: Ayana Nakayama, Tomohiro Hirata, Katsuyoshi Tsujita

Published in: Artificial Life and Robotics | Issue 1/2020

Log in

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

In our research, we proposed a system using multi-robot as a gravity compensation system for a ground test of a spacecraft with a deployable structure. The advantage of the system is its low cost and versatility. When the robots support the beam at the nodes, we can expect to simulate the free vibration of the space structure using the proposed system under gravity. In this study, supporting a uniform, flexible beam with vibration was first implemented to verify the performance of the proposed system. Then we investigated the performance of the system applying to the mock-up model of a spacecraft with a deployable structure as a demonstration.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literature
4.
go back to reference Paules G, Luther M (2000) NASA’s Earth science program-increasing science opportunity and payoff through small satellites. Acta Astronaut 46:61–64CrossRef Paules G, Luther M (2000) NASA’s Earth science program-increasing science opportunity and payoff through small satellites. Acta Astronaut 46:61–64CrossRef
5.
go back to reference Esper J, Panetta PV, Ryschkewitsch M, Wiscombe W, Neeck S (2000) NASA-GSFC nano-satellite technology for Earth science missions. Acta Astronaut 46:287–296CrossRef Esper J, Panetta PV, Ryschkewitsch M, Wiscombe W, Neeck S (2000) NASA-GSFC nano-satellite technology for Earth science missions. Acta Astronaut 46:287–296CrossRef
6.
go back to reference Fischer A, Pellegrino S (2000) Interaction between gravity compensation suspension system and deployable structure. J. Spacecr Rockets 37:93–99CrossRef Fischer A, Pellegrino S (2000) Interaction between gravity compensation suspension system and deployable structure. J. Spacecr Rockets 37:93–99CrossRef
8.
go back to reference Xu Z, Guannan Y, Hai H, Xinsheng W (2010) Deployment analysis and test of a coilable mast for BUAA Student Micro-satellite, IEEE systems and control in aeronautics and astronautics (ISSCAA), 3rd international symposium, pp 1339–1332 Xu Z, Guannan Y, Hai H, Xinsheng W (2010) Deployment analysis and test of a coilable mast for BUAA Student Micro-satellite, IEEE systems and control in aeronautics and astronautics (ISSCAA), 3rd international symposium, pp 1339–1332
9.
go back to reference Sawada H, Mori O, Okuizumi N, Shirasawa Y, Miyazaki Y, Natori M et al (2011) Mission report on the solar power sail deployment demonstration of IKAROS. In: 52nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference Sawada H, Mori O, Okuizumi N, Shirasawa Y, Miyazaki Y, Natori M et al (2011) Mission report on the solar power sail deployment demonstration of IKAROS. In: 52nd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference
10.
go back to reference Greschik G, Mikulas MM (2002) Design study of a square solar sail architecture. J. Spacecr. Rockets 39:653–661CrossRef Greschik G, Mikulas MM (2002) Design study of a square solar sail architecture. J. Spacecr. Rockets 39:653–661CrossRef
11.
go back to reference Meguro A (1993) A module concept for a cable-mesh deployable antenna. In: 27th aerospace mechanism symposium, NASA-CP-3205, pp 51–66 Meguro A (1993) A module concept for a cable-mesh deployable antenna. In: 27th aerospace mechanism symposium, NASA-CP-3205, pp 51–66
12.
go back to reference Meguro A, Mitsugi J (1995) Design and analysis of deployable modular mesh structures for a large space antenna. In: 6th European space mechanisms and tribology symposium, ESA-SP-374, pp 319–324 Meguro A, Mitsugi J (1995) Design and analysis of deployable modular mesh structures for a large space antenna. In: 6th European space mechanisms and tribology symposium, ESA-SP-374, pp 319–324
13.
go back to reference Schenk Mark, Viquerat Andrew D, Seffen Keith A, Guest Simon D (2014) Review of inflatable booms for deployable space structures: packing and rigidization. J. Spacecr. Rockets 51:762–778CrossRef Schenk Mark, Viquerat Andrew D, Seffen Keith A, Guest Simon D (2014) Review of inflatable booms for deployable space structures: packing and rigidization. J. Spacecr. Rockets 51:762–778CrossRef
14.
go back to reference Dean W, Sparks Jr, Juang JN (1992) ’Survey of experiments and experimental fascilities for control of flexible structures. J Guidance Control Dyn 15 Dean W, Sparks Jr, Juang JN (1992) ’Survey of experiments and experimental fascilities for control of flexible structures. J Guidance Control Dyn 15
15.
go back to reference Sparks DW, Juang J (1992) Survey of experiments and experimental facilities for control of flexible structures. J Guidance Control Dyn 15:801–816CrossRef Sparks DW, Juang J (1992) Survey of experiments and experimental facilities for control of flexible structures. J Guidance Control Dyn 15:801–816CrossRef
16.
go back to reference Zwanenburg R (1995) The qualification test programme of the ENVISAT solar array mechanism. In: Sixth European space mechanisms and tribology symposium, pp 65–72 Zwanenburg R (1995) The qualification test programme of the ENVISAT solar array mechanism. In: Sixth European space mechanisms and tribology symposium, pp 65–72
18.
go back to reference Schwartz Jana L, Peck Mason A, Hall Christopher D (2003) Historical review of air-bearing spacecraft simulators. J Guidance Control Dyn 26:513–522CrossRef Schwartz Jana L, Peck Mason A, Hall Christopher D (2003) Historical review of air-bearing spacecraft simulators. J Guidance Control Dyn 26:513–522CrossRef
19.
go back to reference Nitta K, Tsujita K, Kishimoto N (2016) Development of a robotic gravity compensation system for the prototype test of spacecraft. In: IEEE/SICE int. conf. of symposium on system integration, pp 272–277 Nitta K, Tsujita K, Kishimoto N (2016) Development of a robotic gravity compensation system for the prototype test of spacecraft. In: IEEE/SICE int. conf. of symposium on system integration, pp 272–277
20.
go back to reference Abe M, Natori MC, Higuchi K, Shiogama Y (1998) Behavior of space membrane at retrieval phase. J Jpn Soc Civ Eng 598(I–44):247–256 (in Japanese) Abe M, Natori MC, Higuchi K, Shiogama Y (1998) Behavior of space membrane at retrieval phase. J Jpn Soc Civ Eng 598(I–44):247–256 (in Japanese)
Metadata
Title
A study of a gravity compensation system for the spacecraft prototype test by using multi-robot system
Authors
Ayana Nakayama
Tomohiro Hirata
Katsuyoshi Tsujita
Publication date
29-10-2019
Publisher
Springer Japan
Published in
Artificial Life and Robotics / Issue 1/2020
Print ISSN: 1433-5298
Electronic ISSN: 1614-7456
DOI
https://doi.org/10.1007/s10015-019-00568-4

Other articles of this Issue 1/2020

Artificial Life and Robotics 1/2020 Go to the issue