Skip to main content
Springer Nature Link
Log in

Control Parameters Optimization for Spacecraft Large Angle Attitude Based on Multi-PSO

  • Conference paper
  • First Online:
Intelligence Science and Big Data Engineering. Big Data and Machine Learning Techniques (IScIDE 2015)

Part of the book series: Lecture Notes in Computer Science ((LNIP,volume 9243))

  • 2820 Accesses

Abstract

In order to meet the requirement of spacecraft large angle attitude maneuver, the paper presents a spacecraft parameters design and optimization methods for large angle attitude and rapid maneuver. Firstly, Lyapunov controller model is described by quaternion with the output torque of the actuator as constraint condition. Then, the optimal time and power consumption are regarded as the optimized objectives. Finally, a multi-objective particle swarm optimization (MOPSO) algorithm is proposed to solve above control parameter optimization problem. Simulations show that the optimized control parameters which satisfy the constraint of the output torque can make the control system with lower consumption, higher stability and better convergence.

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

Access this chapter

Log in via an institution

Subscribe and save

Springer+ Basic
$34.99 /Month
  • Get 10 units per month
  • Download Article/Chapter or eBook
  • 1 Unit = 1 Article or 1 Chapter
  • Cancel anytime
Subscribe now

Buy Now

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

Similar content being viewed by others

References

  1. Wie, B., Barba, P.: Quaternion feedback for large angle maneuvers. J. Guid. Control Dyn. 8(3), 360–365 (1985)

    Article  MATH  Google Scholar 

  2. Pukdeboon, C., Zinober, A.S.I.: Control Lyapunov function optimal sliding mode controllers for attitude tracking of spacecraft. J. Franklin Inst. 349, 456–475 (2012)

    Article  MathSciNet  MATH  Google Scholar 

  3. Huang, Q., Zhang, J.X., Zhang, Q., et al.: Optimization of control parameters based on multi-objective genetic algorithms for spacecraft large angle attitude. Appl. Mech. Mater. 538, 470–475 (2014)

    Article  Google Scholar 

  4. Lu, K.F., Xia, Y.Q., Zhu, Z., et al.: Sliding mode attitude tracking of rigid spacecraft with disturbances. J. Franklin Inst. 349, 413–440 (2012)

    Article  MathSciNet  MATH  Google Scholar 

  5. Liang, J.J., Qin, A.K.: Comprehensive learning particle swarm optimizer for global optimization of multimodal functions. IEEE Trans. Evol. Comput. 10(3), 281–295 (2006)

    Article  Google Scholar 

  6. Jin, J., Zhang, J.R., Liu, Z.Z.: Optimized design of controller parameters for large angle spacecraft attitude maneuver. J. Tsinghua Univ. 49(2), 289–292 (2009)

    Google Scholar 

  7. Zhang, J.R., Wang, Y.: PSO-based controller parameters design for spacecraft. Trans. Beijing Instit. Technol. 30(4), 425–428 (2010)

    MathSciNet  Google Scholar 

  8. Coello, C.A.C., Pulido, G.T., Lechuga, M.S.: Handling multiple objectives with particle swarm optimization. IEEE Trans. Evol. Comput. 8(3), 256–279 (2004)

    Article  Google Scholar 

Download references

Author information

Authors and Affiliations

  1. Key Lab of Advanced Design and Intelligent Computing, Dalian University, Ministry of Education, Dalian, 116622, People’s Republic of China

    Wenbo Zhao, Jianxin Zhang, Qiang Zhang & Xiaopeng Wei

Authors
  1. Wenbo Zhao
    View author publications

    You can also search for this author in PubMed Google Scholar

  2. Jianxin Zhang
    View author publications

    You can also search for this author in PubMed Google Scholar

  3. Qiang Zhang
    View author publications

    You can also search for this author in PubMed Google Scholar

  4. Xiaopeng Wei
    View author publications

    You can also search for this author in PubMed Google Scholar

Corresponding author

Correspondence to Qiang Zhang .

Editor information

Editors and Affiliations

  1. Zhejiang University, Hangzhou, China

    Xiaofei He

  2. Xidian University, Xi'an, China

    Xinbo Gao

  3. Northwestern Polytechnical University, Xi'an, China

    Yanning Zhang

  4. Nanjing University, Nanjing, China

    Zhi-Hua Zhou

  5. Chinese Academy of Sciences, Beijing, China

    Zhi-Yong Liu

  6. Suzhou University of Science and Technology, Suzhou, China

    Baochuan Fu

  7. Suzhou University of Science and Technology, Jiangsu, China

    Fuyuan Hu

  8. Suzhou University of Science and Technology, Jiangsu, China

    Zhancheng Zhang

Rights and permissions

Reprints and permissions

Copyright information

© 2015 Springer International Publishing Switzerland

About this paper

Cite this paper

Zhao, W., Zhang, J., Zhang, Q., Wei, X. (2015). Control Parameters Optimization for Spacecraft Large Angle Attitude Based on Multi-PSO. In: He, X., et al. Intelligence Science and Big Data Engineering. Big Data and Machine Learning Techniques. IScIDE 2015. Lecture Notes in Computer Science(), vol 9243. Springer, Cham. https://doi.org/10.1007/978-3-319-23862-3_2

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-23862-3_2

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-23861-6

  • Online ISBN: 978-3-319-23862-3

  • eBook Packages: Computer ScienceComputer Science (R0)

Publish with us

Policies and ethics