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Eigenvalue Sensitivity Analysis of Aircraft Power System

  • Jianying LiuEmail author
  • Jin Cai
  • Jiawang Huang
  • Zhangang Yang
Conference paper
Part of the Lecture Notes in Electrical Engineering book series (LNEE, volume 582)

Abstract

Many existing literatures are about improving the controller to improve the stability of the power system. However, the discussion of the power system line parameters is little. This paper models the circuit of aircraft power system based on dq transformation method. Based on the stability analysis of the system, the eigenvalue sensitivity of the power system parameters of the power supply system is calculated, and the influence of the parameters of power system on the small disturbance stability of the power supply system is analyzed. Finally, the simulation verified the correctness of the eigenvalue sensitivity analysis.

Keywords

Aircraft power system Modeling Eigenvalue sensitivity Simulation 

Notes

Acknowledgements

This work was supported by the Innovation Team Cultivation Plan of Colleges and Universities in Tianjin (TD13-5071), the Fundamental Research Funds for the Central Universities (3122018D005), Aeronautical Science Foundation of China (20170267002).

References

  1. 1.
    Rosero, J.A., Ortega, J.A., Aldabas, E., et al.: Moving towards a more electric aircraft. Aerosp. Electr. Syst. Mag. IEEE 22(3), 3–9 (2007)CrossRefGoogle Scholar
  2. 2.
    Ciezki, J.G., Ashton, R.W.: Selection and stability issues associated with a navy shipboard DC zonal electric distribution system. IEEE Trans. Power Delivery 15(2), 665–669 (2000)CrossRefGoogle Scholar
  3. 3.
    Zhou, S., Qi, R., Lin, H.: Load stability analysis of multi-electric aircraft power system. Aeronaut. Comput. Technol. 32(4), 93–95 (2002)Google Scholar
  4. 4.
    Lokman, H., Hassan, H., Moghavvemei, M., Haider, A.F., et al.: Optimization of power system stabilizers using participation factor and genetic algorithm. Int. J. Electr. Power Energy Syst. 55(55), 668–679 (2014)Google Scholar
  5. 5.
    Ness, J.E.V., Boyle, J.M., Imad, F.P.: Sensitivities of large, multiple-loop control systems. IEEE Trans. Autom. Control 10(3), 308–315 (1965)CrossRefGoogle Scholar
  6. 6.
    Qianru, X.U., Yong, C.U.I.: Power system stabilizer configuration and parameter tuning based on eigenvalue sensitivity. East China Electr. Power 42(10), 2069–2073 (2014)Google Scholar
  7. 7.
    Liu, X., Lu, S., Guo, Q., Xia, D.: Calculation of sensitivity of eigenvalues to operation mode. Autom. Electr. Power Syst. 22(12), 9–12 (1998)Google Scholar
  8. 8.
    Zhou, E.Z.: Functional sensitivity concept and its application to power system damping analysis. IEEE Trans. Power Syst. 9(1), 518–524 (1994)CrossRefGoogle Scholar
  9. 9.
    Gibescu, M., Christie, R.D.: Quadratic sensitivities for power system steady-state control. IEE Proceed. Gener. Transm. Distrib. 144(3), 317 (1997)CrossRefGoogle Scholar
  10. 10.
    Areerak, K.: Modelling and Stability Analysis of Aircraft Power Systems. University of Nottingham (2009)Google Scholar

Copyright information

© Springer Nature Singapore Pte Ltd. 2020

Authors and Affiliations

  • Jianying Liu
    • 1
    Email author
  • Jin Cai
    • 1
  • Jiawang Huang
    • 1
  • Zhangang Yang
    • 1
  1. 1.College of Electronic Information and AutomationCivil Aviation University of ChinaTianjinChina

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