Skip to main content

Formation-Keeping Control of the Closed-Chain System

  • Chapter
  • First Online:
Theory and Applications of Multi-Tethers in Space

Part of the book series: Springer Tracts in Mechanical Engineering ((STME))

  • 424 Accesses

Abstract

The three-body closed-chain system cannot achieve the ideal LP equilibrium state under uncontrolled state, the main reasons are that there are slack and rebound phenomena in the tether between the three spacecraft, which is due to the low rotational rate of the tether system in the initial condition of LP equilibrium and the inability of the tether to withstand the pressure.

This is a preview of subscription content, log in via an institution to check access.

Access this chapter

eBook
USD 16.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 109.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 109.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. Wertz JR, Larson WJ (1999) Space mission analysis and design. California Microcosm Press, El Segundo

    Google Scholar 

  2. Kumar KD, Yasaka T (2004) Rotating formation flying of three satellites using tethers. J Spacecr Rocket 41(6):973–985

    Article  Google Scholar 

  3. Huang PF, Hu ZH, Meng ZJ et al (2015) Coupling dynamics modelling and optimal coordinated control of tethered spacerobot. Aerosp Sci Technol 41(2):36–46

    Article  Google Scholar 

  4. Wang DK, Huang PF et al (2014) Coordinated control of tethered space robot using mobile tether attachment point in approaching phase. Adv Space Res 54(6):1077–1091

    Article  Google Scholar 

  5. Wang DK, Huang PF et al (2015) Coordinated stabilization of tumbling targets using tethered space manipulators. IEEE Trans Aerosp Electron Syst 51(3):2420–2431

    Article  Google Scholar 

  6. Huang PF, Zhang F, Ma J (2015) Dynamics and configuration control of the maneuvering-net space robot system. Adv Space Res 55(4):1004–1014

    Article  Google Scholar 

  7. Huang PF, Hu ZH, Zhang F (2016) Dynamic modelling and coordinated controller designing for the manoeuvrable tether-net space robot system. Multibody Syst Dyn 36(2):115–141

    Article  MathSciNet  Google Scholar 

  8. Vogel KA (2006) Dynamics and control of tethered satellite formations for the purpose of space-based remote sensing. Air Force Institute of Technology, Ohio

    Google Scholar 

  9. Williams P (2006) Periodic optimal control of a spinning earth-pointing tethered satellite formation. In: Proceedings of the AIAA/AAS astrodynamics specialist conference and exhibit, Keystone, Colorado, America

    Google Scholar 

  10. Mori O (2007) Formation and attitude control for rotational tethered satellite clusters. J Spacecr Rocket 44(1):211–220

    Article  Google Scholar 

  11. Hussein I, Schaub H (2009) Stability and control of relative equilibria for the three-spacecraft coulomb tether problem. Acta Astronaut 65(5):738–754

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Panfeng Huang .

Rights and permissions

Reprints and permissions

Copyright information

© 2020 Springer Nature Singapore Pte Ltd.

About this chapter

Check for updates. Verify currency and authenticity via CrossMark

Cite this chapter

Huang, P., Zhang, F. (2020). Formation-Keeping Control of the Closed-Chain System. In: Theory and Applications of Multi-Tethers in Space. Springer Tracts in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-15-0387-0_7

Download citation

  • DOI: https://doi.org/10.1007/978-981-15-0387-0_7

  • Published:

  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-15-0386-3

  • Online ISBN: 978-981-15-0387-0

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics